- .Lr 4. gm? 4.2.5 mfi . c 2.. a fin. .s _ h.“ .. Wfiww , . v... N flwfi. ... 3.. 1...». . .mm. “Mu” a.“ 3.. .... 2...... H:.fi....ca..... “23.52:. , E. Au. ...:. 23.: 5am? . . , magi? . . $5 {2% ' . a?» . {IQ-cop nu .. . ~ ! E .3 amwhfivr VI :21: A . .. ... ,....nm.......=§. .r! a: .3: 3.1. have Hannah. .. as .. .. .u.:....% ,5... 1...... dad .. ,1. ‘0 1.. sturuvvl 1. 175.27 I a. .l . .51 :1 :u. n I :2 y. n12r..uud 1., .1. .6... .t .! é ‘ .L...» 9.3 ....f t . v I. . v 3.1).: £ylft)..!7 .1 .1: Ila-DI . It .. 3 . n h.-\ \1 I c a . 3.. «.833... lllllllllllllllHill)“Ill”!!!lllllllllllllllUl 01046 0552 This is to certify that the dissertation entitled IMPROVING ENGINEERING SYSTEM DESIGN THROUGH SCIENTIFIC VISUALIZATION METHODS presented by GAYLE ELLEN ERMER has been accepted towards fulfillment of the requirements for PH . D . degree in MECHANICAL ENGINEERING WW Major professor 0 Date rl-r/VOV 4% MS U is an Affirmative Action/Equal Opportunity Institution 0-12771 LIBRARY l Michigan State University — PLACE II RETURN BOXtomnavothi-chockoutmnmm TO AVOID FINES Mum on or More data duo. DATE DUE DATE DUE DATE DUE I MSU lsAn mm ActioNEmd Oppommity Inuituion mm: *— IMPROVING ENGINEERING SYSTEM DESIGN THROUGH SCIENTIFIC VISUALIZATION METHODS By Gayle Ellen Ermer A DISSERTATION Submitted to Michigan State University in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Mechanical Engineering 1994 ABSTRACT IMPROVING ENGINEERING SYSTEM DESIGN THROUGH SCIENTIFIC VISUALIZATION METHODS By Gayle Ellen Ermer One of the greatest challenges for designers of complex engineering systems is to interpret simulation data. Numerical results need to be presented in a way which is meaningful and encourages understanding Of the simulated system behavior. Scientific visualization (SV) is an emerging discipline in which methods are developed for clear presentation of data to scientists and engineers. This thesis presents a significantly improved design environment for engineering systems which has been developed and implemented using the concepts of SV . The design environment is based on the Bond Graph (30) as a modeling representation. The 36 captures the interconnectedness of the system components and Shows power pathways as energy is transferred within the system. Animation of Simulation results directly on the BG and the correspondence between the bond graph model and the physical system are both exploited to aid the designer in comprehending the system’s behavior. The research was conducted in two phases for each of which pilot environments were designed. In phase one a two-dimensional animation tool for simulation of variable values on the 86 was developed (BGVis-2D). A complex railcar airbrake switching system was modeled and simulated to illustrate the benefits of the visualization. A second example was developed to show the application Of the new visualization tool in a somewhat abstract model space, namely modal analysis . In phase two a tool to represent 805 as 3-D objects was developed using the PHIGS graphics standard (BGVis-3D). A bounce-pitch-roll model of a car body and suspensions was implemented in the 3-D environment and its simulated behavior when encountering a pothole was investigated. Dedication To my husband, Eric. iv ACKNOWLEDGEMENTS I would like to sincerely thank my major professor, Dr. Ronald Rosenberg, for his support, guidance, and encouragement throughout my PhD. program. Not only was his knowledge invaluable for my research, but I learned many things about teaching from him as well. I also express my appreciation to the members of my thesis committee: Drs. Clark Radcliffe, Erik Goodman, and Richard Hall gren. Their suggestions and comments were very valuable. My gratitude also extends to ASME for providing me a graduate teaching fellowship and to the Zonta organization for awarding me the Amelia Earhart Fellowship. These scholarships were very precious to me, not only financially, but in the encouragement they gave me to continue pursuing this degree. Finally, special thanks go to my parents, Robert and Carol Essenburg, and the rest of my family for always encouraging me to use my talents and for instilling in me the values that made this accomplishment possible. TABLE OF CONTENTS List of Tables ...................................... viii List of Figures ..................................... ix Nomenclature ..................................... xii Chapter 1 - Introduction ................................ 1 1.1 Problem Definition ............................. 1 1.1.1 Importance of Improving the Efficiency of System Design . . . 1 1.1.2 The Role of Insight and Interpretation of Results ........ 2 1.1.3 The Role of Visualization in the Modeling Process ....... 5 1.2 Research Objectives ............................ 11 1.3 Description of Thesis Organization .................... 14 Chapter 2 - Bond Graphs and Scientific Visualization ................ 16 2.1 Using Bond Graphs as a Tool for System Analysis and Design ..... 16- 2.1.1 Modeling of Engineering Systems ............... 16 2.1.2 Bond Graph Modeling Methodology .............. 19 2.1.3 Computer Support for Simulation ................ 23 2.2 Scientific Visualization .......................... 24 2.2.1 Description of the Field ..................... 24 2.2.2 Current Tools and Research Areas ............... 27 Chapter 3 - A Two-Dimensional Bond Graph Visualization Environment ..... 30 3.1 Environment Specifications ....................... 30 3.2 Design of the Two-Dimensional Visualization Environment ...... 31 3.2.1 Features Selected for Implementation ............. 31 vi 3.2.2 Platform Selected for Implementation ............. 38 3.2.3 User's Guide ................... , ....... 40 Chapter 4 - A Three-Dimensional Bond Graph Visualization Environment ..... 45 4.1 Environment Specifications ....................... 45 4.2 Design of the Three-Dimensional Visualization Environment ...... 46 4.2.1 Features Selected for Implementation ............. 46 4.2.2 Platform Selected for Implementation ............. 48 4.2.3 Description of the PHIGS Graphics Standard ......... 49 4.2.4 User's Guide ........................... 53 Chapter 5 - Visualization Examples Using BGVis-2D ................ 57 5.1 Automobile Modeling Example ..................... 57 5.2 Railcar Airbrake Switching System Example .............. 79 5.3 Modal Analysis Example ........................ 110 Chapter 6 - Visualization Example Using BGVis-3D ................ 116 Chapter 7 - Conclusions ............................... 122 7.1 Summary of Contributions ....................... 122 7.1.1 Two-Dimensional Visualization ................ 122 - 7.1.2 Three-Dimensional Visualization ............... 123 7.2 Areas for Further Research ....................... 124 Appendix A - A Brief Introduction to Bond Graph Modeling ........... 128 Appendix B - Program Documentation and Code ................. 139 8.1 Two-Dimensional Environment ..................... 139 8.2 Three-Dimensional Environment .................... 203 Appendix C - Example Model Files ......................... 254 References ...................................... 271 vii LIST OF TABLES Table 1. Standard Bond Graph Elements ..................... 22 Table 2. Car Body and Suspension Model Equations and Parameters ...... 65 Table 3. Response Data from Pothole Simulation ................ 67 Table 4. Eigenvalues/vectors of Mechanical Three DOF System ........ 112 Table A-1. Variables in Various Energy Domains ................ 129 Table A-2. Standard Bond Graph Elements ................... 130 Table A-3. Block Diagram Elements ....................... 130 Table A-4 Causality Possibilities for Bond Graph Elements ........... 13S viii Figure 1. Figure 2. Figure 3. Figure 4. Figure 5. Figure 6. Figure 7. Figure 8. Figure 9. Figure 10. Figure 11. Figure 12. Figure 13. Figure 14. Figure 15. Figure 16. Figure 17. Figure 18. Figure 19. figure 20. Figure 21. figure 22. LIST OF FIGURES A Design Process Description ..................... 4 An Engineering Simulation Activity Diagram ............. 5 Interpretation of Results Diagram ............... . . . . 1 1 Scientific Visualization and the Design Process ............ 27 Dynamic Display Key to Widths and Colors .............. 36 ENPORT Postprocessor Module Control Window ........... 40 Dynamic Display Module Control Window .............. 41 PI-IIGS Modeling Transformation Pipeline ............... 52 3-D Postprocessor Control Window .................. 53 The 3-D Postprocessor Display Window ............... 56 Vehicle System Illustration .................. . . . . 58 Schematic of Car Chassis Unit and Suspensions with Seat ...... 59 Macro Bond Graph of BPR Model .................. 60 2-D Bond Graph Representation of Seat Unit ............. 61 2-D Bond Graph Representation of Rigid Chassis Unit ........ 62 Detail of Single Suspension Assembly ................ 63 Two-Dimensional Bond Graph of Car Model ............. 64 Mathematical Model of Pothole Source of Flow ........... 66 Response Data from Pothole Simulation ............... 68 Power Variable Response for BPR Model (Time = 0.050) ...... 70 Power Variable Response for BPR Model (Time = 0.110) ...... 71 Power Variable Response for BPR Model (Time = 0.115) ...... 72 ix Figure 23. Power Variable Response for BPR Model (Time = 0.135) ...... 73 Figure 24. Power Variable Response for BPR Model (Time = 0.300) ...... 74 Figure 25. Power Variable Response for BPR Model (Time = 0.305) ...... 75 Figure 26. Power Variable Response for BPR Model (Time = 0.325) ...... 76 Figure 27. Glyph Display of Energy Response for BPR Model (Time = 0.135) . 77 Figure 28. Time Plot of Displacement Obtained by Selecting Q88 ....... 78 Figure 29. Schematic of the Airbrake Control Valve Switch ........... 80 Figure 30. Top Level Bond Graph Decomposition ................ 81 Figure 31. Bond Graph Decomposition of DB- 10 Module ............ 82 Figure 32. Schematic of the Service Accelerated Release Valve (2) ....... 83 Figure 33. Bond Graph of the Service Accelerated Release Valve ........ 84 Figure 34. Power Variable Display for Check Valve (Time = 0.5) ....... 87 Figure 35. Power and Effort Variable Display for Check Valve (Time = 0.76) . 88 Figure 36. Flow Variable Display for Check Valve (Time = 0.21) ........ 89 Figure 37. Flow Variable Display for Check Valve (Time = 0.6) ........ 90 Figure 38. Bond Graph of the Main Piston System and Reservoirs ........ 92 Figure 39. Power Response for Air Brake Model Charging Mode (Time = 18.9) 94 Figure 40. Power Response for Air Brake Model Charging Mode (Time = 31.8) 95 Figure 41. Power Response for Air Brake Model Charging Mode (Time = 49.8) 96 Figure 42. Power Response for Air Brake Model Charging Mode (Time = 58.2) 97 Figure 43. Figure 44. Figure 45. Figure 46. Power Response for Air Brake Model Braking Mode (Time = 12.9) . 99 Power Response for Air Brake Model Braking Mode (Time = 14.1) . 100 Power Response for Air Brake Model Braking Mode (Time = 19.95) 101 Flow Response for Air Brake Model Recharging Mode (Time = 2.85) 103 Figure 47. Flow Response for Air Brake Model Recharging Mode (Time = 5.4) 104 Figure 48. Flow Response for Air Brake Model Recharging Mode (Time = 9.45) 105 Figure 49. Flow Response for Air Brake Model Recharging Mode (Time = 14.4) 106 X Figure 50. Figure 51. Figure 52. Figure 53. Figure 54. Figure 55. Figure 56. Figure 57. Figure 58. Figure 59. Figure 60. Figure 61. Power Response for Air Brake Model Release Mode (Time = 2.25) Power Response for Air Brake Model Release Mode (Time = 4.2) Schematic of Mechanical Three DOF System ............. Bond Graph of Mechanical Three DOF System ............ Flow Variable Display Showing First Mode Shape .......... Displacement Variable Display Showing Second Mode Shape . . . . Displacement Variable Display Showing Third Mode Shape 3-D Bond Graph Representation of Car and Suspensions Model 3-D Dynamic Display Of Response to Pothole Input (Time = 0.112) . 3-D Dynamic Display of Response to Pothole Input (Time = 0.115) . 3-D Dynamic Display of Response to Pothole Input (Time = 0.300) . 3-D Dynamic Display of Response to Pothole Input (Time = 0.305) . Figure A-1. Mechanical Translation Example .................. Figure A-2. Figure A-3. Figure A-4. Figure A-S. Figure A-6. Figure A-7. Electrical Example .......................... Hydraulic Circuit Example ...................... Schematic of Radar Pedestal Control System ............ Section (Macro) Bond Graph as Illustration of Decomposition . . . Bond Graph of the Radar Pedestal System . ............ Response to a Step Input ....................... xi . 108 109 110 111 113 114 115 117 138 NOMENCLATURE cg - Center of Gravity e - Voltage E - Effort F - Flow F - Force i - Current P - Momentum P - Power Q - Displacement t — time V — Velocity w - Rotational velocity ABBREVIATIONS AR - Auxiliary Reservoir BC - Brake Cylinder BG - Bond Graph BP - Brake Pipe CV - Check Valve ER - Emergency Reservoir SV - Scientific Visualization xii Chapter 1 Introduction 1.1 Problem Definition 1.1.1 Importance of Improving the Efficiency of System Design Today's competitive global markets put a great deal of pressure on engineers to efficiently design, manufacture, and maintain engineering systems. It is no longer sufficient to produce systems which are adequate. In the future, engineers must be concerned with achieving the "best” design to meet specifications by improving device performance and eliminating undesirable behaviors. They must produce new products in the shortest possible amount of time in order to stay competitive. They also need to know how much variation in the designed system's behavior can be tolerated to determine manufacturing constraints. The design process is intended to produce an optimum solution to a problem through iteration (Arora, 1989). This is becoming an increasingly difficult task as engineering systems become larger in scale and span many different engineering disciplines. Automobiles and aircraft are important examples of complex systems which require detailed prediction and assessment of system function to generate improvements in Performance and reductions in undesired behaviors such as noise. Studying system behaVior by modeling the system with experimental physical prototypes is a time consuming and expensive method for design enhancement. Some systems, such as the 2 proposed National Aerospace Plane designed to fly at speeds up to Mach 25, may be impossible to study to any great extent in this way. Therefore, it is necessary to improve the practice of design by making it easier to predict and comprehend the behavior of engineering systems. Mathematical modeling and simulation of physical systems is one of the most cost effective methods for analysis and prediction of system behavior, especially for systems of very large scale. The trends of the future require mathematical modeling and simulation which promote learning and understanding about system behavior to allow engineers and designers to make changes which improve a system. This dissertation describes research to improve engineering system design through the development Of tools that improve the efficiency and effectiveness of the design process. 1.1.2 The Role of Insight and Interpretation Of Results Considerable thought has been given to the subject of what components should be included in a design methodology and the order in which they should be executed. Some current views of the process of designing will be briefly described in order to set the Stage for a system design progression which shows clearly some areas where improvements would be welcome. In his book The Principles of Design, Suh specifies a design method which begins with the identification of "function requirements" from a given societal need. A product is created and its behavior is compared to the functional requirements. The product is then modified iteratively until the functional requirements are satisfied (Suh, 1990). Medland prOposac a computer-based design process which consists Of three main phases: concept, analysis, and scheming. These processes are interconnected and information can flow 3 between any pair of them (Medland, 1986). Shoup defines a more precise six-step process Of design which includes: recognition of need, creating a design, preparing a model, testing and evaluating the model, improving the design, and communicating the design. These activities form a control loop of sorts where the design is improved until it passes the testing and evaluation stage (Shoup, et a1, 1987). Manufacturability is also a key element in the design of systems, and recently much attention has been given to how this concept should be integrated into the design process (Gadh and Prinz, 1991). These models of design synthesis, along with others in the literature, can be helpful in identifying where improvements to this process are needed. In order to provide a common framework within which the improvements to the design process described in this thesis can be detailed, a description of design practice has been developed which is specific to lumped parameter system design. Figure 1 presents a general design process description which involves several information objects. This particular diagram is only one view of the process of system design selected from the many which have been proposed, but it covers the main features of this activity as described by others, and it gives a basis for the figures and discussion which follow. The aim of an engineering design process is to fill a given societal need either by inventing a physical system to solve some problem, or by improving the performance of a given System. In this context, the designer's model is the mental picture the designer has of the Strueture and behavior of the physical object which constitutes the engineering system. In the Case where the design is only conceptual, the internal model is the designer's perception of the components and behavior of the resulting design. The designer's model is the“ inherently hard to identify or control, since it exists only in the mind of the designer. The activity of design involves relating several concrete inf orrnation objects to the desi guer’ 3 model in order to provide knowledge about potential system improvement and Opt“ . lm‘Zation. One information Object is the specified behavior for the system to be 4 designed, which may be numerical or qualitative. Although the relationship between specified behavior and modeling is very important, the examination of this aspect of design is not the focus of this research. Another information object is the measured behavior. This would consist of any experimental lab testing which reveals information about the behavior of the system. Obviously if the design is only in the conceptual stage, there may not be data of this type available. The remaining information state is the simulated behavior of the system. This is information which can be obtained from mathematical modeling and analysis. This research is concerned with the shaded area of the diagram, which has been labeled analysis activity. The focus is on the interaction between the reference model in the engineer's mind and the knowledge which (an be gained through the activities of modeling and simulation. It is the improvement of the relation of these two information objects that is Valuable in leading to optimization of the design. Figure l. A Design Process Description. a; 3 1.1.3 The Role of Visualization in the Modeling Process Figure 2 shows a more detailed Simulation activity diagram which focuses on the analysis portion of Figure 1. This particular process outline is based on the use of system or bond graphs as a structured modeling technique. The nodes in the diagram are model information states, while the connectors represent transfonnations of information from one state to another. Paths between the nodes other than the ones actually drawn in the diagram exist, but were omitted for clarity. A brief description of each of the Steps in Figure 2 follows. Some of the current computer tools available to support these stages are also mentioned. l (6) Visual Display 0? Behavior 13 2-3 5-6 (5) Numerical Characterization 1-4 (3) System Graph Model of Behavior V 34 (4) Equation Model 4-5 FIgure 2. An Engineering Simulation Activity Diagram 6 Designer's Model (node I ). The first step in physical system analysis is to mentally identify the particular system under consideration. This mental model is primarily visual and has been described as "the mind's eye, the locus of our images of remembered reality and imagined contrivance" (Ferguson, 1992). Building this model includes identifying the boundaries of the system and important system variables, as well as comprehending and visualizing the basic relationships among system components. All characteristics of the system significantly affecting the behavior must be included in the designer's reference model; otherwise the results of the model simulation will not be accurate. In physical systems of realistic complexity, some relatively unimportant characteristics may have to be neglected in order to make the problem manageable. Schematic model (node 2). The next Step typically involves making further assumptions about system characteristics and sketching the Operational ones on paper or on a computer screen in a form which is commonly understood. This process is associated wi th path 1-2 in Figure 2. The schematic model is an idealization of the physical system Which includes all important aspects of system behavior to be considered, and it is usually domain specific. For example, mechanics has its own symbols for commonly used items such as springs, masses, dampers, and the connections between them, while electrical engineering has developed a standard set Of circuit diagramming techniques. At this point the Schematic model is an iconic one (Suckling, 1978). That is, it represents the physical SyStem components and interconnectedness in a Spatial way without holding to actual dimensions, but clearly the schematic corresponds to the topology of the actual system. For some simple design problems it may be possible to form an equation model directly from kno“(ledge of the physical system, following a path from 1 to 4, but this is not usually pra“meal for complex systems. The problem with Obtaining an equation model from schernatic information, following a path from 2 to 4, arises because different parts of a large m - . “1 tldisciplinary system are expressed in domain-specific modes, Wthh leaves no easy ‘ .7 method for a consistent translation to the form of a mathematical model which will allow simulation. Hence the use of bond graph methods becomes desirable for multidomain engineering systems. Software applications do exist which facilitate the transition from domain Specific schematic models to mathematical models directly. Circuit modelers such as PSPICE (PSPICE User Manual, 1989), mechanical multibody systems analyzers such as ADA MS (ADAMS User’s Manual, 1989), finite element solvers such as ANSYS (ANSYS User's Manual, 1993), and hydraulic software packages like PipeFlo (Shearing, 1992) all fall into this category. For example, using ADAMS it is possible to create 3-D solid models of rigid bodies and their connectors with a graphical editor, and then to animate the mathematically simulated motions of the system on a computer monitor. Such a display is very helpful in giving the designer a feel for how the design will move under different conditions. These types of software are of great benefit in designing their respective single-discipline systems, but they are not sufficient for use when integrating several disciplines into one system design. System Graph Model (node 3). In order to put all the pans of the system model in a unified form, a system graph model can be constructed, as in path 2-3. System or bond graph modeling is a standardized modeling approach which deals with energy transfer between model components (Karnopp, Margolis, and Rosenberg, 1990). It sets up a framework into which systems from most domains of engineering can be translated. Information in the form of control signal and block diagram elements can also be included, in which case the bond graph becomes a system graph. A system graph is a topological model, presenting the components of a system and their connections with no regard as to their actual geometry or spatial placement. The advantage of developing a system bond graph is that a complete operational mathematical model of the system behavior can easily 8 be obtained, and computer support is available for this task. However, the disadvantage of formulating the model in bond graph form is that the apparent correspondence between the model and the physical system is weaker than it is with a schematic. A two-dimensional system graph representation requires visualization effort on the part of the designer when he or she is considering the behavior of a three—dimensional physical system. Computer software exists which can aid the engineer in creating and manipulating bond graph models as well as in deriving equation models and in calculating numerical solutions. One particular program is ENPORT, which has been designed to implement bond graph modeling techniques (Rosenberg, 1993). The bond graph elements and structure can be input by using a two-dimensional graphical editor. Another bond graph modeling environment is CAMAS (Broenink, 1990). CAMAS is an interactive computer language developed to implement bond graphs. The graphical editing capabilities also permit bond graph development represented in two dimensions. Equation Model (node 4). A mathematical equation model contains all relevant quantitative information about a system in question. The equation model allows prediction of the responses of an engineering system to various conditions without implementing them physically. For lumped parameter systems, the mathematical models generally consist of sets of ordinary differential equations. However, for many designers, there is very little conceptual correspondence between a three-dimensional physical system and a set of equations. The abstractness of this type of model is what generates the need for intermediate modeling techniques like schematics and bond graphs. It is also very difficult to compose the large sets of equations required to describe complex systems without a structured graphical model. Equations can be generated automatically from system graph models (path 3-4) using ENPORT or from discipline-specific schematics using programs like PSPICE. Numerical Characterization of Behavior (node 5). At this point the model building task is complete. Given the equation model, computers can be used to perform the simulation (path 4-5), usually by solving the mathematical equations iteratively, since most practical problems do not have closed-form solutions. Various algorithms exist which are capable of performing this task. As real-world systems design is becoming increasingly complex, continuing increases in computational speed and memory size allow for more and more data to be generated related to a system under analysis. Many computer programs exist for general numerical solution of equations. These facilitate the creation and solution of equation models obtained from physical systems or schematics and can be identified as direct equation or block-diagram type programs. Examples of these are the MATRIX-x software environment (MATRIX-x User’s Guide, 1990), and MATI-IEMATICA, a powerful mathematical symbolic equation solver (Wolfram, 1991). These programs provide two and three dimensional output, but variables are not necessarily directly related to the physical system. Difficulty in using these programs is also encountered when the systems to be analyzed are very large involving many mathematical equations. Programming in this case can be extremely complicated. Many single-discipline modeling programs such as PSPICE have their own solvers based on commonly used algorithms. ENPORT and CAMAS also have their own built-in equation solvers. Visual Display of Behavior ( node 6). A critical part of the simulation process is to take the resulting response data from a numerical simulation and interpret it in a meaningful way so that the physical system itself can be better understood (path 6-1). This involves both quantitative analysis of simulation results and qualitative analysis leading to understanding of global system function. The important features of the system response 10 need to be highlighted. A designer who understands how a system behaves will be equipped to make the right changes to improve the design. Rosenblum and Brown call this process "realization" (Rosenblum and Brown, 1992). Appropriate displays of system response can greatly improve the interpretation of results process. Figure 3 shows some of the possible ways to relate visualization to model information states in order to apply simulation results to the designer's conceptual model. The designer visualizes system response in terms of (2), (3), or (4) depending upon which model building strategy was used. If the system is single-domain and has an accepted iconic representation (e. g. rigid bodies or electronic circuits), then the most useful display is the link between (6) and (2); this is denoted (A) in Figure 2. This type of display has been implemented in many domain-specific computer programs. For example, ADAMS shows motions of rigid bodies; PSPICE displays currents related to electric circuit diagrams. Linking the results directly to the equations (C) would allow plotting of variables versus time or cross-plotting of variables, one versus another. Often, however, the degree of abstractness of an equation model makes visualization difficult. Path (B) can be followed to link simulation results data with the system graph in a display which could Show system variables (e.g. powers, energies, forces, currents) directly related to the system graph. By linking results data directly to the system graph in a computer environment, the engineer can take advantage of the structure provided by the bond graph model to understand the overall meaning of the results data. It is this visualization process that is enhanced by the work described here. The usefulness of a coherent design package based on the bond graph modeling technique which aids in all steps of the design process, especially the interpretation step, is becoming clear. ll (1) Designer's Model (2) Schematic Model 66) Visual Display oh Behavior (3) System Graph ModeD (5) Numerical Characterization of Behavior ((4) Equation 14on Figure 3. Interpretation of Results Diagram 1.2 Research Objectives The principal objective of this research was to create and implement a Si gnif icantly improved design environment for engineering systems based on the use of bond graph methods as a structured modeling technique. A common practice in the context of dynamic system analysis is to build a system graph model, to choose a set Of parameters for defining the constitutive equations of each of the elements of the model, to run a numerical simulation of the model for given initial conditions, and finally to compare the output results to the expected or required behavior. In this way an engineer can determine if the model is behaving properly (model verification). Once the model is verified, the engineer can experiment with changing parameters to improve the system performance compared to the design requirements for the output response. The types of questions asked by the designer after a simulation might be: Which subcomponents of the model are most important in determining overall system behavior? Which components use very little power and might 12 be eliminated to reduce the computational order of the model? Which parts of a mechanical model move the largest distances over the course of a dynamic response? Which voltages in the electrical part of a model fluctuate the most and do they remain within required levels? DO the power levels of all the elements stay within reasonable limits for the chosen parameters and initial conditions? A major goal of this research was to design an environment which makes the interpretation of dynamic system response easier for designers and makes answering these types of questions as straightforward as possible. This objective was met in two separate stages, for each of which prototype softwares were implemented. The first stage concentrates on improving the interpretation of simulation results by providing a power-related animation directly tied to the 2-D system graph. Current 2-D bond graph computer models were enhanced to provide time-varying power information on the system graph. Computer animation is a natural way of visualizing time-varying results obtained from a simulation. The animation shows global patterns of behavior as well as focusing on individual quantitative details Upon demand. Energy transfer and/or other variable value information being indicated by color and line-width variation or glyph-type symbology as an animation in time was explored. The line-width variation technique has previously been implemented in ENPORT to display time-averaged power variables on the system graph (Rosenberg and Zhou, 1988). This approach was extended to dynamic display of time-varying quantities on the system graph, thus providing an energy and information-based animation of the system behavior. Various scaling options are made available to the user to provide for selection of a scaling which most clearly Shows the dynamics of the energy propagation in the system. A method was developed for representing the changing direction of each energy flow. Other display codes were also used which involve changes in glyph drawings to reflect the energy change in a node with time. Once these concepts were studied in a 2-D environment, they were applied to the next phase. 13 The second stage involved building a pilot environment for using three-dimensional system graphs. Three-dimensional visualization is necessary because better correspondence between topological system graph models and actual physical systems or schematics will help the designer apply his or her physical intuition to a model in a more meaningful way. A topological model in general is helpful because it conveys the relationships between variables in the system, but it lacks a direct relationship to the spatial characteristics Of the system. An engineer can conceptualize about a physical system because it can be pictured visually in space, but at the point where a two-dimensional bond graph model is constructed, direct correspondence to the physical system is lost to a large degree. In this work, a system graph was allowed to be more than a topological model alone. A graphical environment was developed in which system graph display can correspond directly to the geometric imagery of the physical problem. The concept can be thought of as 'true geometry' in the sense that a three-dimensional system graph can be a scaled representation of a physical system with its elements fixed to the spatial positions of the matching elements of the physical system. Capability for dynamic rotation Of the display was provided in order to achieve an actual three-dimensional effect (Hays, 1992). The user is also allowed to manipulate the model as a geometric object in the computer environment. The result is better visualization of the power flow pathways captured in the three-dimensional structure of the bond graph. The principles of the emerging field of scientific visualization as expressed by some of its proponents (T ufte, 1983 and 1990, Cox, 1990) were used to make the visualization of each stage clear and easily understandable. In the past, traditional methods have been successful in providing knowledge of system behavior to designers, but the production of ever larger, more complex, and interdependent systems require substantially improved design methods like the ones described here, in order to promote comprehension and 14 learning. This work makes a significant contribution to the area of complex system design by providing a new tool for engineers which complements existing tools. Since the nature of the project is closely tied to computers and their ability to produce color graphics and animation, color printouts and photographs are included in this thesis wherever possible, and a videotape of the example systems as implemented in the pilot 2-D and 3-D computer environments is available upon request from the author directly or through the Mechanical Engineering Department of Michigan State University. 1.3 Description of Thesis Organization This thesis consists of the sections described in this paragraph. The current chapter contains an introduction to the problem and motivation for the research as well as the order or Presentation of further contents. Chapter 2 contains background information relevant to the problem, in particular a short description of bond graphs and a discussion of scientific visualization principles and practice. Chapter 3 includes a complete description of the two dimensional visualization environment created in answer to the problem statement. Chapter 4 Covers the extension of bond graphs to a three-dimensional representation and visualization of results in the three-dimensional environment. Chapter 5 illustrates the use of the designed environment for solving some problems of practical scale, namely an air- brake switching system and a car and suspension model. It also contains a discussion of how the designed environments can be used in educational situations. Finally, Chapter 6 p’eSents a summary of what was accomplished and some ideas for future development. Appendices are included which contain more details on certain topics related to this thesis. Appendix A includes a more comprehensive explanation of bond graph modeling for readers who are not familiar with the techniques. More details on the Structure and coding or the visualization software implementations are shown in Appendix B. The complete description of the Air-brake Switch bond graph model and its equations. as well as the 15 ENPORT model files for both the car and suspensions example and the air-brake switching system, are included in Appendix C. This document concludes with a list of references of particular use in carrying out this research. Chapter 2 Bond Graphs and Scientific Visualization 2.1 Using Bond Graphs as a Tool for System Analysis and Design 2.1.1 Modeling of Engineering Systems In the introductory chapter of this thesis the importance of modeling in the process of designing a physical system was emphasized. Models exist in many different forms, but in all cases their purpose is to convey to an engineer as much information about the System's behavior as possible, and to provide the information in such a way that the underlying concepts behind the behavior are clear and insight into the problem is gained. An engineer cannot design a system without a reasonable conception of the way the system oPetates and the influence that parameters have on the behavior. Certainly it is possible to learn a great deal about a system's behavior by building and running tests on the system itself. Usually this is not a practical way to approach d‘Sign and it is not the most efficient. Once a system has been built, it is very expensive to make the changes in the design that might be necessary in order for it to meet performance critearia. Optimization in this situation is very difficult. Scaled models of systems, which Presumably represent the behavior of a larger system but on a smaller scale, can also be use51.111 in yielding insight about the system. Unfortunately, these types of models (wind tunnel mockups, for example) incur some of the same disadvantages as full-scale Pmtorypes. They are still very expensive and time-consuming to build and are hard to modify once they have been built. 16 17 In order to learn about system behavior without building physical prototypes it is very useful to construct mathematical models of systems. This practice is often called “virtual prototyping” (Puttre, 1992), Since the idea is to identif y the behavior of a system within a computer environment in order to replace or supplement what can be learned about system behavior from the construction of physical prototypes. These virtual prototypes or models capture the physical behavior of the system in their structure and can be simulated to provide information about the system's response to different inputs and changes in system characteristics. The mathematical models used to represent lumped parameter systems typically occur as sets of ordinary differential equations. Parameters in the equations can easily be changed to reflect design modifications, and unnecessary hardware costs are avoided. Solving the equations numerically for given initial conditions and parameters over a certain time period provides a prediction of the actual response of the system, and if the Virtual prototype accurately captures the important aspects of the behavior of the system, it can then be used to see the effect of changes in the parameters or conditions under which the system is operated. In this way the design of the system can be improved and Optimized. Unfortunately, obtaining a set Of mathematical equations for a system of realistic complexity is not a very straightforward task and can be prone to error. The large number or Variables and parameters involved, along with the complex relations between those Variables, make the problem difficult to approach. To make the transformation from Physical system to equations easier, various types Of graphical modeling systems are used. Gmphical modeling can be seen as a “bridge between the mathematics of differential e(Nations and the physics of engineering systems” (Rosenberg and Kamopp, 1983). GraPhical models are easier to understand in terms of the connectivity of the various parts of the system model than are the equations. Graphical models are more closely related to 18 the geometry of the original system. They are appropriate for managing the information in large-scale systems in a hierarchical way. In general, the more removed an engineering model representation is from the geometric form of the physical system, the harder it is for an engineer to understand it intuitively. Different types of graphical modeling are involved in the process of going from a physical system to a set of mathematical equations. One type is the schematic diagram. Schematic diagrams help to capture the attributes of a system in order to make equation derivation easier, but quite often schematic diagrams are not precise enough in the definition of variables to make the process of equation formulation exact and unique. For instance, in mechanical schematics, often certain assumptions are not made clear in their structure, such as whether friction applies to a given motion or not, or whether heat losses from a Component are important and should be considered. It is also difficult to connect schematic models which have been constructed in different engineering disciplines, Since the notations are quite different in each. For example, in mechanical schematics certain symbols are commonly used to represent masses, springs, and dampers. In electrical schematics certain SYmbOIS represent resistors and other electrical circuit elements. However, the connections bflween these two different schematic domains are not well defined in either terms. Another common graphical modeling system is the block diagram. Block diagrams clearly indicate the existence of functional relationships among variables in the system, but the structure of the graph does not take into account the physics of the problem in a direct way unless the entire system is signal-based. Block diagrams are closer to mathematical equation models in that they Show variables directly as the connectors and represent functional relationships by the nodes (i.e. blocks). Bond Graphing is a very useful modeling technique which can be used to avoid Some of the problems associated with both schematic diagram models and block diagram .-~ if? 3 71¢ "‘ " “t." 'l‘l tr‘ -.. H -§Li. 4 'rt. .54“ I 19 models. Bond Graphs are topological in form and therefore provide a close relationship between the physical device and the model, while still providing a clear representation of functional relationships in the model which can be translated directly into mathematical terms. Bond graphs are especially valuable in cases where the system to be considered spans more than one energy domain because they can represent energy transduction in a graphically consistent manner. A brief description of bond graph modeling methodology is included in the next section. 2.1.2 Bond Graph Modeling Methodology Bond graphing is a Structured modeling technique used to represent multi-domain SYStems as a series of components linked by power bonds. The systems best modeled by b0nd graphs are lumped parameter systems which can be mathematically modeled as sets of Ordinary differential equations. Bond graphs provide a basis for detailed physical modeling 0f engineering systems in preparation for simulating their behavior. The graphs capture the flow paths for energy within a system in a way which agrees with the underlying physical laws of the components (Karnopp, et a1, 1990). Some examples of bond graph models can be seen in chapter 5, where the visualization examples are described. Additional examples appear in a brief introduction to using bond graphs for system modeling included in Appendix A. Bond graphs support hierarchical decomposition of large-scale systems by dividing them into subcomponents and connections at different levels. Each of the connections represents an energy transfer, or power, at that connection. The power is the product of a Pair of variables, denoted effort and flow. If consistent units are used, power units can be equated across different engineering domains (e. g. watts). Energy measured consistently can then be seen to flow through the connectors from one domain to the other. This is one 20 feature that makes bond graphs useful for modeling multi-domain systems. It keeps the bond graph much closer to the physics of the system than a block diagram, which does not track energy flow directly. An additional characteristic of bond graphs is that they are highly organized in the representation of information in the model. The bond graph modeling process can be followed in a very structured way, which makes model building clearer and less prone to error and confusion. Bond graphs are also very precise statements of which model effects are included. They make clear all of the assumptions made in the modeling process at the energy level. They do not indicate the functional details of the effects. At the lowest levels of a bond graph decomposition of a system, a relatively small set 0f bond graph elements can represent the physical behaviors present in a remarkably broad set of components and effects. Bond graph techniques recognize the similarity of physical behaviors across different energy domains and use this energetic similarity to produce Concise, unified models. For example, in electric circuits a linear resistor behaves as a device which drains power (P) from the circuit at a rate equal to the current (i) in the resistor multiplied by the voltage (e) in the resistor (P = i*e); correspondingly in a mechanical SyStem a viscous damper also dissipates power from the system and does so at a rate of the Velocity (V) multiplied by the force (F) in the damper (P = V*F). The constitutive ecIllations for these two effects are the same and bond graphs take advantage of that fact to Produce coherent models. Although this example demonstrates linear relationships between var‘iables, non-linear effects can readily be represented by bond graphs also. The process of using bond graphs to model a system often enhances the modeler's knowledge of the System and can also yield insight into the system’s behavior, even before simulation has been performed. 21 The set of standard bond graph elements includes several element or node types. These are shown in Table 1. Source elements supply energy to the system. Passive elements describe observed types of physical behaviors, such as the dissipative effect mentioned above. Two—port elements support the modeling of energy transformation from one domain to another. Junction elements serve to connect these elements together in a way which is consistent with the physical laws governing the behavior of the component. Each element has its own constitutive equations which describe the behavior of that element. These equations can be either linear or non-linear. Once a complete bond graph of a system is constructed using these elements, causality can be added to graphically indicate which variables are inputs and which are outputs within the system. Bond graphs can also be combined with block diagram elements and Si gnals to allow for the study of different types or control structures and their effect on system behavior. A bond graph that integrates Control signals through block diagrams with bonds is called a System Graph. System graphs support the direct formulation of a set of state Space equations from the model. State space equations are a useful form for doing system analysis or control design. At this point the equations can be numerically solved and simulations can be run for various test conditions. A critical part of the system analysis process is to take the Faulting response data from the numerical simulation and interpret it in a meaningful way. Advantage Should be taken of the structure provided by a bond graph model in the display of the numerical results of a simulation, since the bond graph already has a special c0lTespondence to the physical system in the designer’s mind. 22 Table 1. Standard Bond Graph Elements. Element Element Bond Graph Constitutive equations Type Name Symbol General Form Linear Form B Sources Source of SE ——>‘ E = f (time) E = Constant Effort F Source of SF __E_;. F = 1“ (time) F = Constant Flow F Passive - 4f__ - _ a: One—Ports Resrstance R F E — f (F) E — R F , E E=f(Q) E=l/C*Q Capacnance C ‘7— F = dQ/dt F = dQ/dt . E V=f(P) V=l/L*P Inertia I ‘———F E = dP/dt E = dP/dt 1“” 1'1 El E2 E1 = n * E2 O'PO Transformer -——‘ T ——-‘ transducers F1 {-2 F1 = l/n * F‘2 E1 E1 = r * F2 _.3 ____.x q; Gyrator Fl GY F2 F1 = I“. 3 E2 E1 E3 _. .. Junction One-Junction —-‘ 1———‘ F1 ’ F1 " F3 elements F1 E2 LE2 F3 E1-E2-E3 = 0 El [-3 Zero-Junction —F—3 07—3 E1 = E. = E3 ‘ ELK! ‘ F1-F2-F3=O 2.1-3 Computer Support for Simulation Computer support for the activities of modeling and simulation is necessary to enable practical design work. The typical activities involved in simulating system response are selecting appropriate parameters for all of the constitutive equations of the bond graph model, then solving for the dynamic response for some selected initial conditions. The purpose of the simulation at first might be to see if the model performance matches the expected performance. This is the model verification stage. Once the model has been shown to behave properly, it can be used to test the system performance's sensitivity to changes in parameters. The response can be optimized according to some performance criteria. A variety of output data types can be used to generate information about the model's behavior, such as time-history data, linearization and eigenvalue data, steady-state Values, and sensitivity of these values to system parameter changes. Several valuable services are provided by computer simulation to make the process or design iteration and optimization more efficient. The first is that computers can be used to remove the tedium of deriving the actual ordinary differential equations sets, and to make coIlStr'uction and modification of models easier. Mistakes can also be avoided which might Occur in equation derivation due to the complexity of the problem. With good computer SnPport, the user can concentrate on modeling and design decisions, since the computer can hilndle the updating of equations as changes are made. Second, computers are useful in numerically solving the mathematical model, since most problems of practical size do not have closed form solutions. Third, one of the most important functions of the computer in System modeling and simulation is in the capability it provides for display and examination of results data. Computers allow the user to explore the data, looking at in from different perspectives so as to gain insight into the system behavior. 24 Bond graph models lend themselves to algorithmic derivation of the system equations. Therefore computer support for bond graph modeling can be provided and system behavior can be simulated effectively at the detailed numerical level. For example, the ENPORT software accepts bond graphs and block diagrams as components in an integrated modeling environment (Rosenberg, 1993). ENPORT makes construction and modification of system graphs a straightforward graphical process, as well as supporting the equation derivation and solution processes. ENPORT can also be used to display the results data in X-Y plots of variables versus time. Display of time-averaged power variables is directly on the bond graph as color and line-width variation of the bond structure (Zhou, 1988). This may not be adequate if transient phenomena are considered, which is quite often the case in complex system design. It is also possible to pass the equations from ENPORT in symbolic form to other software that can interpret the equations; this is another level of manipulation that can lead to insight 2.2 Scientific Visualization 2.2. 1 Description of the Field Scientific visualization, also referred to as data visualization, is emerging as a means t0 help answer the need for clearer ways of presenting response data to designers. As ever mOre powerful computers and measuring instruments generate ever more data, we face a need for more effective ways to interpret and use that data. One definition of scientific visUalization is "using computer-generated graphics to help us understand and visually Clarif y the relationships inherent in data" (Rosenblum and Brown, 1992). Another is that scientific visualization "uses computer generated images to help scientists extract knowledge and understanding from experimental or simulated data" (Nielsen, 1993). A National Science Foundation report was recently published which encouraged engineers and 25 scientists to develop new visualization methods to promote both research and education (McCormick, DeFanti and Brown, 1987). NSF also recently awarded $14.6 million to establish the National Science and Technology Center for Computer Graphics and Scientific Visualization, illustrating just how much importance is placed on progress in this area. The research reported upon here is an attempt to meet this challenge in the specific area of dynamic engineering systems design. Scientific visualization addresses the problem of data interpretation by combining several different computer-related disciplines. Scientific visualization depends on computer expertise relating to graphics and information processing, as well as on expertise related to the different scientific domains in which visualization is used. There is also an artistic component that involves aesthetics, and a biological component involving theories of human perception. How humans perceive things and what is meant by understanding are issues that are not entirely defined at this time. The field of human perception attempts to explore these iSsues by observation and experimentation. This field relates directly to scientific Visualization because knowing how humans relate to data and the physical world around “mm is a prerequisite to creating the most effective design and simulation environments. Like a computer, a human undergoes a specific process used to internalize information. Unlike a computer, this process is somewhat hard to identify. If some aspects of this Process are examined, information can be organized in such a way as to take the best advantage of human information processing capabilities. It has been shown that data which are organized in a structured fashion are understood and remembered better that data presented in an unorganized manner (Haber and Wilkinson, 1982). It has also been shown that humans are capable of comprehending 26 more complex concepts visually than through words and numbers alone (Haber and Wilkinson, 1982). The visual system provides a way to organize even non-pictorial data in a geometric structure. Various studies have shown that the natural way for people to relate to data is pictorially. Visual data is remembered better than words or numbers (Standing, Conezio, and Haber, 1970), and our visual systems automatically attempt to interpret fiat pictures as if they are real geometries in three dimensions. Another facet of human perception is that humans tend to remember and relate to data better when they have control over their manipulation of the data. This is why user- driven interactive visualization is a goal to be striven for. There are also certain ways of presenting data which distort the human perceptual process and can be used to trick the user. Although there is no motivation to distort data in an engineering modeling problem, Since the goal is accurate understanding of system behavior, care must still be taken to avoid unintentionally presenting data in a way which might be misinterpreted. Obviously, a good design and simulation environment should avoid any possibility cf confusion. For engineering modeling and simulation, scientific visualization provides a way to make interesting features of the simulated behavior stand out rather than be obscured by numerical data. The challenge of applying the concepts of scientific visualization in a design context is to create computer-aided visualization environments which help engineers ‘0 comprehend the physical significance of their simulation models' behavior. The idea of Visualization can also be applied in engineering education, where visual thinking and mental in'lagery need to be stressed in order to promote better understanding of engineering fnnclamentals. Scientific visualization concepts can be used to support better understanding of b0nd graph model analysis by providing two types of capabilities. These are illustrated in 27 Fr gure 4 where the connection between the designer's model, the bond graph model, and the visual display of model behavior is highlighted. The first capability involves presentation of data obtained from simulations by relating the response directly to the bond graph structure (Path Y). The second capability increases the correspondence between the bond graph model and the designer's models, and therefore the physical system, by associating the bond graph with the system geometry in three dimensions (Path X). 2.2.2 Current Tools and Research Areas The field of scientific visualization is used in many different scientific domains and in a variety of ways. Applications are found in disciplines as diverse as medicine, meteorology, engineering, architecture, computer programming, physics, chemistry, statistics, and mathematics. These applications range from the simple display of two- dimensional scatter plots to complex‘three—dimensional mappings of data to geometry. < (l) Designer's Model > X Y (6) Visual Display of Behavior ((2) Schematic ModeD ((3) System Graph Model) (5) Numerical Characterization of Behavior ((4) Equation Model Figure 4. Scientific Visualization and the Design Process. 28 One of the major areas of current development in scientific visualization is the display of continuous or sampled data in two or three dimensions. This visualization process involves a series of transformations which provide a mapping between raw data and certain graphical element attributes. Some examples of programs which support the display of general distributed data values are: l) PV-Wave (Schmalzel, 1992), which includes 2-D line and scatter plots, 3-D contour and surface plots, as well as table and animation data views; 2) Data Visualizer by Wavefront Technologies (Brittain, 1990), which can handle distributed fully structured as well as unstructured data; 3) AVS, a commercial module-based visualization system (Upson, 1989); 4) Visage, which supports distributed visualization (IEEE Visualization, 1992); and 5) the equation solvers like MATHEMATICA and ANSYS previously mentioned. Such programs require the user to decide on a visualization method and to direct how the raw data will be displayed. It was decided that these stand-alone general visualization softwares were not sufficient for the required bond graph design environment although they are complementary. The structure supplied by the bond graph model should be exploited for understanding as fully as possible. Another area which is being extensively studied is distributed system visualization known as scenic or quasi-scenic rendering (Becker and Cleveland, 1991). The goal of this type of visualization is to map information obtained from experiments or simulations onto their associated distributed geometric surfaces or volumes. This covers areas such as volume visualization of medical data (Fuchs, et a], 1989) and computational fluid dynamics (Giles and Haimes, 1990). Similar techniques are being applied to stresses and strains in engineering mechanics (Haber, 1990). Although distributed parameter systems, which in a modeling context involve the Solution of partial differential equations, have been and are being extensively explored by 29 scientific visualization techniques, less has been done in the area of spatially lumped or finite dimensional systems, which involve the solution of time dependent ordinary differential equations. Imaging methods are needed in this area to provide as much detailed information to designers as possible within a global context that corresponds well to the graphical model and the physical problem. For this research an area of application for scientific visualization principles has been identified which has not been explored up to this time, namely the application to bond graph modeling and display of simulation data. The structure of this type of visualization is lumped, rather than distributed over a volume, since the positions of nodes and connectors have been defined, and the goal is to use this structure to do modeling that relates to physical systems and to display data in a meaningful way. The display can be thought of as a problem of high-dimensional data, since 3 physical dimensions (x, y, z) are dealt with as well as time and the values of the variables of interest. The topic of display of high dimensional data has not been an area of a lot of research, perhaps because it is so complex. The research that has been done includes the use of iconic representations like Chemof f faces (Chemof f , 1973), and some work which is concerned with showing a dependent variable which is a function of many independent variables (Beshers and Feiner. 1992 and Mihalisin, et a1, 1991). The bond graph output display problem is somewhat different in that it is necessary to show the values of many dependent variables (associated with the powers on all the connectors of the bond graph) as a function of time in the context of their position in the bond graph model. Chapter 3 A Two-Dimensional Bond Graph Visualization Environment (BGVis-ZD) 3.1 Environment Specifications The goal of this visualization environment is to relate the response data calculated by a solution of the system equations obtained from the bond graph model to the structure of the bond graph model. The response is usually determined by a numerical solution of the equations, but could be obtained from a closed-form solution in the case of linear systems. Since the designer presumably understands how the bond graph model relates to the actual physical system under study, this will organize the output data in a way that is highly consistent with the designer’s understanding of the physical system. Since bond graphs are designed to capture power paths within a system, some useful quantities to display will be the power and energy values. What is needed is a way to display the instantaneous value of a variable type for each of the bonds in a system graph as an animation in time. The common method for displaying results from a bond graph model simulation consists of plotting one or a small number of variable values versus time on a two- dimensional screen or hardcopy. Output from block diagram or direct mathematical equation model solutions are displayed in this same way, indicating that the structure of the bond graph itself is not being utilized in any way to aid in the organization and Presentation of the output data. This approach also requires that the user choose the Variables of importance for display. This implies some prior knowledge or expectation of 30 31 which elements in the system need to be checked, which may not always be obvious. Displaying a larger number of variables in an organized fashion would allow the significant aspects of the global system behavior to become clear. Then relevant variables can be identified and plotted if the user requires more detailed information. One existing possibility of taking advantage of the bond graph structure for displaying data is the option of displaying time-averaged variables in a static display as line width and color variation on the bond graph (Zhou, 1988). This type of presentation is very helpful in separating sections of the graph which demonstrate high versus low averages of variables, which might lead to model reduction, but it is not necessarily adequate for dealing with the interpretation of transient system response. The Zhou method of average value presentation can be used as a base to extend the display of variable values to a dynamic animation in time. The visualization environment should be smoothly integrated as part of a data post-processor into a bond graph model building and solving environment. As much control of the display as possible should be given to the user to allow him or her to interact with the data in ways that are most meaningful. The user interface should, of course, be clear and easy to understand and manipulate. 3.2 Design of the Two-Dimensional Visualization Environment 3.2.1 Features Selected for Implementation The variable types chosen for potential display on the bond graph are the power variables, effort and flow, as well as the power variable itself, and also the energy variables displacement and momentum, as well as the energy variable itself. Effort (E) 32 and flow (F) variables for each bond over every time stage in the time range of solution are obtained from the simulation and stored in the results file. Power (P) variables for each bond are calculated in the dynamic display postprocessor by multiplying the effort and flow on each bond for each time stage. The momentum (P) and displacement (Q) variables are not stored as a result of the simulation, except for those that are state variables. In order to calculate all of the P and Q variable values over the solution time range, the fact that effort and momentum and flow and displacement are related by the integral relationships P -fE dr+ Po, and Q -der+Qo , respectively, was used. A trapezoidal integration routine was implemented to calculate the momentum variable from the effort variables for each time step, and the same procedure was used to calculate the displacement variable from the flow variables for each time step. The following equation defines the trapezoidal integration. Ema. Pg-[x(.0).2x(r,).2x(.2).....2.(.,,_ l).,.(i,,)] For the integrations, all of the initial values for displacements and momentums were taken to be zero. Instantaneous energy variables were determined by integrating the product cf the flow and effort on each bond for each time step. Once the variable values over all the bonds for the time range of interest are available, each variable type is checked for global maximum and minimum values, and magnitude ranges are determined. This allows each variable type to be scaled consistently over all bonds. Three types of scaling options are available: linear, logarithmic and absolute logarithmic. The logarithmic scaling options normally are useful when values of a variable type extend over several orders of magnitude. Logarithmic scaling can only be used if all variable values for the variable type to be displayed are greater than zero. The dynamic display checks for this condition, and prints an error if an attempt is made to scale negative or zero-valued data logarithmically. 33 Absolute logarithmic scaling uses only the absolute magnitudes of the values, where the negative sign on the value is indicated by the arrow direction or color change. Thus the problem of negative numbers is avoided. Zero values are set to the minimum magnitude value for the variable type to avoid the error associated with taking the logarithm of zero. Bond Coding. The two primary modes for time varying display of bond related variables are line width variation of each bond and color variation of each bond. This method can be thought of as "flow" display, as opposed to ”level" display which is described under the heading of Node Coding. Line width variation and color variation methods can be used independently, allowing two different variable types to be displayed at once, or they can represent the same variable type, thus providing reinforcing display variations for the same variable type. Ten levels of difference variation are provided for the line width modulating feature. The choice of this number was affected by the geometry of which the display device is capable. A maximum line width was determined by the relationship of bonds to nodes in the presentation of the graph, while the minimum line width was determined by the minimum line width allowed in the line drawing routine. After some experimentation, it was determined that ten gradations of line width between the maximum and the minimum provide the user with variation sufficient to detect meaningful differences in variable values. Negative values for a given variable are indicated by a shift in the arrow placement on the bond for linear and absolute logarithmic scaling methods. This is an especially natural way to think about power flow, since by definition power flow on a bond is positive in the direction of the half arrow. 34 Ten levels of color variation are also provided. This number could be increased for more detailed data display since human perception of color variation is more sensitive than perception of geometry differences. When line width and color are used to show the same variable type, only one set of colors, shaded from purple to red, is used, since the arrow directions indicate negative results. When color and line width are used to represent separate variables, two sets of color are used, the same as above for positive values, and a set shaded from green to blue for negative values. The two distinct color sets allow the negative versus positive data to show up very clearly. Another possibility is to use the VBGYOR (rainbow) spectrum to show value level change, but it is not clear that this color set is always intuitive for people in comprehending the corresponding levels, and the position of a zero-valued level is not obvious. For each time stage of the animation, the bonds are redrawn with the appropriate width corresponding to the variable value type selected for line-width and the appropriate color corresponding to the variable type selected for color. Node Coding. During a results display the nodes of the graph are drawn once in the colors originally defined by the model builder relating to energy domain: white for general, blue for mechanical, green for electrical, purple for hydraulic, and so on, as defined in the ENPORT model building module (Rosenberg, 1992). A secondary visualization tool that is supplied in the BGVis-2D tool, associated with nodes or ”levels" rather than bonds or ”flows”, is a glyph symbol located at each C, I and R node in the graph. This method can be used by itself or in combination with the previously described ”flow" type display. A glyph is a geometric symbol that represents information at a given position. The glyph is based on a thermometer motif and shows the amount of energy stored or dissipated in that element at a given time. The energy increase or decrease is shown by an increase or decrease of the line height in the 35 thermometer-style glyph. The glyph technique might also be extended to include display of other variable types that can be viewed as ”levels", such as displacement. The net energy transfer to any node in a bond graph can be determined by integrating the instantaneous power values on each of the bonds connected to that node and summing the results. The C and I elements are known as energy storage elements because the amount of energy stored in the element can be determined from the net energy transfer plus the addition of any initial energy already stored in the node. The user is allowed to supply a numerical value for the initial energy stored in each C and 1 element. The amount of energy dissipated in an R element is determined directly from the net energy transfer. The glyph display at these nodes can be useful for the designer trying to understand where energy is being accumulated and released throughout the system globally during a simulation. Signal Coding. Signals are not included in the dynamic display of power, energy, effort, flow, momentum, or displacement variables, since the power flow along a signal is by definition equal to zero, and because there is no consistent way to indicate to which variable type the information carried by a signal belongs. If bond graph builders were encouraged to label signal values with the first letter of the label corresponding to the variable type (E, F, P, or Q), then a method might be set up to include the apprOpriate signals when a given variable type is displayed. At this point, signal variable values can be displayed independently from bond variables by choosing to display a ”signal" variable type. A key is provided to indicate the correspondence between line widths and colors and numerical value levels. An example of the key is shown in Figure 5. Each line width is drawn in the first column, and the range of numerical values it represents is indicated 36 above and below it. In the second column, each color is demonstrated, both negative and positive, and the numerical values corresponding to that color are printed. In the case where no variable is chosen to be displayed with line width variation, the line widths are drawn without numerical labels. Similarly if no variable is chosen for color variation, the colors are still shown, but are also unlabeled. The key is updated whenever new variable types are chosen for display as either line width or color variation. At the bottom of the key, the value of the time for which the data is currently being displayed is shown. This value is updated whenever the time step displayed is changed. Pos Neg 0.00E+00 0,00£+00 IIIIIIIII 1.296-01 1.33E+03 III-III- 2.58£-01 2.67E+o3 IIIIIIIII 3.87E-01 4.00E+03 — — 5.168-01 5.34E+03 _ — 6.455-01 6.67E+03 IIIIIIIII IIIIIIIII _ — 9 038-01 9 34Eeo3 IIIIIIIII lull-III- 1. 03E+00 1.07E+04 — 1.16E+00 1.20E+04 - 1.29E+00 1.33E+04 Figure 5. Dynamic Display Key to Widths and Colors. 37 Time Plots. The graphical variation methods described above are intended to be qualitative in nature, dealing with relationships between the values of variables at different locations within the entire bond graph. At some point it may become useful to zoom in on variable values associated with a particular bond. This function has been provided by allowing the user to select a bond in the dynamic display, whereupon the user is allowed to choose one of the bond variables for display in a plot as a function of time. An even more precise display might focus on choosing a particular point in time from the time plot for a particular variable and obtaining numerical values for variables in table form. This function has not yet been implemented in the dynamic display environment, but a similar result can be obtained by using the "table” function provided outside of the dynamic display environment. Time plots of several chosen variables related to different bonds in the graph can also still be constructed by using the facility provided in the original ENPORT postprocessor. Animation Control. A user may desire to display the results of a simulation over the entire time frame used in the solution of the differential equations or over some subset of that time. The choice of time subsets for the simulation data is provided by the ENPORT postprocessor. The determination of ranges for each variable type is performed over this chosen time frame. The user also requires a way to control the rate at which the animation is presented. Time controls are provided for this task. Several options have been implemented. The user is allowed to run the display from the current time to a later time specified by the user at a constant speed (seconds per frame) that is input by the user. During this constant speed animation, no user input is allowed. In order to account for a user who might not want to proceed through the animation at a fixed rate, single time step functions are provided. These functions allow users to proceed with the animation at 38 their own pace by selecting a button to move forward or backward one step. A function is also provided to allow users to quickly go to a specified time stage without having to step through all the intermediate stages. View Control. A user of the BGVis-2D environment might also wish to display only a portion of a bond graph model if the model is so large that the display will be cluttered. The ability to pan through the graph in both the x and y directions is provided by scrollbars attached to the graph viewing window. It is also possible to zoom in to or out from a graph view. 3.2.2 Platform Selected for Implementation The bond graph modeling program ENPORT was chosen as the vehicle for implementation of the environment characteristics described above. ENPORT was described in the previous chapter as a software environment which accepts bond graphs and block diagrams as components in an integrated modeling environment, makes construction and modification of system graphs a straightforward graphical process, and supports the equation derivation and solution processes. ENPORT was chosen because it is a well-documented and verified software program, and because the software code was available in a convenient setting for modification and addition of visualization functionality. ENPORT is currently available in three different formats. An earlier version is written in FORTRAN and runs on mainframe computers which run the VMS operating system. At the time this research took place, the VMS operating system was being gradually phased out. The most common currently distributed version of ENPORT is written in FORTRAN and runs on MS-DOS based personal computers. An experimental 39 version of ENPORT is implemented in a UNIX environment and is programmed in the C computer language, taking advantage of the X Window System user interface. The UNIX version of ENPORT was chosen for the addition of the new display technologies of this research for several reasons. The mouse-driven X Windows format provided better user interface characteristics when compared to the other versions, which are more menwdriven. What is more important, the higher processing requirements of the graphics display anticipated, especially for the 3-D capability, required the power of a workstation. It is planned that the display enhancements generated by this research will eventually be carried over into the PC environment, especially since 486 and Pentium processors are becoming more widely used by engineers. The implementation of this research was performed on a Sun Spare-10 workstation running the UNIX operating system. The ENPORT version used was the 1.0 8 version running under UNIX. All additional code was written in the C computer language, and the Xt Intrinsics functions, along with the Athena widget set, were used to support the user interface functions (Nye and O'Reilly, 1990). Documentation and the computer code generated in the course of the project are included in Appendix B of this report. The enhancements to the bond graph modeling environment were added as part of a postprocessor module of ENPORT. Examples of how the BGVis-ZD environment described in this chapter is actually used for visualization purposes are described in chapter 5. The figures provided in that chapter provide a rough idea of a process that is inherently dynamic and interactive. There is a videotape available from the author directly or from the Mechanical Engineering Department at Michigan State University which provides a clearer indication of how the designed bond graph visualization environment actually performs. 3.2.3 User's Guide The following section can be used as a reference for running the software implementation of the BGVis-2D tool. Each of the available functions is described in the order in which it would most likely be performed. Pictures of the user interfaces are included. Starting the Postprocessor. The ENPORT program's postprocessor window is started by typing the name of the postprocessor program, which is "BGVis-ZD". This interface can be used to load in simulation results files, provide 2-D plots of selected variables versus time, specify time intervals of interest, and start the animation module. A picture of the control window is shown in Figure 6 for reference. Exiting the ENPORT postprocessor can be executed by clicking on the "Exit" button at the appropriate time. Figure 6. ENPORT Postprocessor Module Control Window. i5 is; 41 Loading an Output File. Clicking on the "Load" button will bring up the directory structure window which will allow the user to select an ENPORT simulation output file (suffix .SZP) previously generated by the ENPORT solver module. Clicking on the file name will then cause that file to be loaded into the postprocessor. Selecting a Time Interval. The default time limits shown in the initial and final time boxes are taken as the beginning and ending times of the simulation (see Figure 6). If some subset of that time interval is desired for study, new time limits can be entered into the boxes by simply typing them in using the keyboard. . Elly-Iii??? E'Z'X" ' '2'1‘3-2'2'2'2‘ ("i-2+9:iii-319?};-1'2 u‘h'{I}!.fi‘n‘h'$#.'lu‘$:£'.VM‘A¥:':'-'Ifl.‘n'u'Na’d'J-‘ERJ- J' .a:-' ‘ .‘V-‘(u‘u Figure 7. Dynamic Display Module Control Window. 42 Entering the Dynamic Display Module. Clicking on the button labeled ”Dynamic Display" will initialize the Dynamic Display Dialog. A picture of this control window is shown in Figure 7 for reference. Loading the model file. Clicking the "Load" button at the top of the menu area at the far left will bring up the same file selection window as in the postprocessor. This window can be used to select the ENPORT model file (suffix .ENP) to be loaded. This file contains the system graph as constructed in the ENPORT model build module. The system graph will then be drawn in the animation viewport, scaled so that the model fits in the window. Determination of output variable ranges occurs at the time of model f ile loading. Using the Animation Viewport. The large window in the dynamic display dialog is the canvas on which the system graph is drawn. There are two functions included related to controlling the appearance of the graph. The first allows the user to shrink or increase the size of the model by clicking the "Zoom” button at the bottom left of the dialog. Doing so will bring up a window into which a chosen scale factor can by typed via the keyboard. The second involves using the scrollbars at the bottom and to the right of the window to pan through the model. Choosing variables for display. The choice for which of the seven variable types (power, effort, fiow, energy, momentum, displacement, signal, none) to display for line width and which one to display for color are made by mouse selection from pull-down menus provided at the top of the dynamic display control window (see Figure 7). Clicking and holding in the box to the right of the menu label will cause the pulldown menu to pop up, and the mouse can be dragged down and released on the appropriate variable option. The user can choose whether or not to display the glyphs during an 43 animation by using the “Show glyphs?" pulldown menu also at the top of the dynamic display window. Choosing a Scaling Method. The program allows three choices for scaling of variables: linear, logarithmic, and absolute logarithmic. The choice of which to use is governed by the pull-down menu obtained when the button next to the "Scaling Choice" label is clicked and dragged down to the appropriate choice and then released. If negative values of the chosen variables are present when logarithmic scaling is chosen, an error message will be shown. Controlling the Animation. The controls for running the dynamic display are included in the box at the top right of the dynamic display dialog labeled ”Animation Control Menu” (See Figure 7). When the "Animate" button is chosen, the dynamic display is drawn for each time increment from the current time to the time specified by the user at a speed (seconds per frame) that is input by the user. The fastest rate available is 1 second per frame and the user can choose any multiple of that as the approximate rate of display by typing into a popup window. During the time this animation is being performed, the display updates automatically, and no interference by the user is allowed. in order to account for a user who might want to control the animation by moving one frame at a time, “Step forward” and “Step backward" functions are provided. These functions allow the animation to proceed either forward or backward by one time increment when the button is clicked. If the current timestage is the lower time limit, and ”Step backward” is chosen, no action is taken. Similarly, it the current timestage is the upper limit, no action is taken. A “Go to timestagez” function is also provided to allow the animation to be redrawn at the specified time stage without having to step through all the intermediate stages. Clicking on this button will pop up a box into which the desired time value can be entered by the user. Interpreting the Data Key. The smaller viewport window on the right is provided to show the numerical scale values of the displayed variables that correspond to each color and line width possibility. The current time stage value is also displayed at the bottom of this window. Obtaining a Time Plot for a Bond. If a detailed plot of a variable associated with a single bond is desired, it can be obtained by clicking on the bonds name in the animation viewport. The user is allowed to specify which variable type will be displayed (power, effort, flow, energy, momentum, displacement, signal). This pops up the plot window, with the selected variable for that bond displayed as a function of time. Time plots of several variables can be displayed by returning to the ENPORT postprocessor control window and using the "Plot” button. Leaving the Dynamic Display Module. Click on the ”Exit" button in the menu area at the far left to close the window and exit the dynamic display module. This will return the user to the postprocessor where a different results f ile can be located, or the program can be exited. Chapter 4 A Three-Dimensional Bond Graph Visualization Environment (BGVis-SD) 4.1 Environment Specifications As was shown in the previous chapter, there are definite advantages to be gained from relating the response data from a simulation directly to the bond graph. These advantages are extended with the ability to display bond graphs in a three-dimensional environment and to manipulate them as 3-D geometric objects. The basic goal of the three-dimensional bond graph modeling environment is to make the viewing of power pathways or other variable values easier and to make interpretation of the model behavior clearer. An example of this type of thinking in the area of chemistry/physics is the visualization of complex molecular structures. This type of visualization is generally conducted for the purpose of interpretation of molecular behavior (Mof fat, 1991). In a similar manner, more insight into a bond graph model can be gained if the designer can interact with it in such a way that it can be visualized in three dimensions and the viewing process can be under the modeler's control. The BGVis-3D environment allows for viewing of the 3-D graph from different angles and from a range of distances. The user is able to position the graph in the way that makes its structure and behavior the most clear. The same specifications related to controlling the data presentation in the animation that were presented for the 2-D situation also apply here. The intention of the environment is also to allow the user to display a bond graph model which corresponds closely, allowing for scale, with the three-dimensional 45 46 geometry of the physical system being designed. Bond graphs are usually described as a topological modeling type, meaning that the connectivity of the graph does not generally relate to the geometry of the physical object. This can be an advantage, since the subcomponents of the bond graph model can be moved in whatever way seems suitable without changing the character of the model, as long as the correct connectivity is maintained. The disadvantage of a topological model is that it does not encourage visualization of the geometry of the physical system in the modeling process. The ability to use a three-dimensional geometric bond graph gives the model a well-defined spatial relationship to the physical object, allowing the designer to understand the model behavior in light of the actual geometry of the system. The environment allows for animation of variable types on the bonds in much the same way as for the 2-D environment, but the results can be even more clearly related to the physical system in the 3-D environment. 4.2 Design of the Three-Dimensional Visualization Environment 4.2.1 Features Selected for Implementation The bond graph is displayed in the 3-D environment with spheres as nodes and cylindrical solids with cone-shaped arrows as bonds. Although standard bond graph convention calls for a half-arrow to indicate bond direction, full arrows are used in the BGVis-3D display. The primary reason for this choice is that any arrow that does not extend out in all directions from the cylindrical bond might not be seen if the graph is viewed from a particular orientation. To avoid any ambiguity in interpretation of connector type, signals are displayed as rectangular solids, distinguishing them from cylindrically shaped bonds. Bond graph nodes are drawn as spheres, while block diagram elements are drawn as rectangular solids. The nodes are drawn in colors corresponding 47 to their power domains, while the connectors have changing colors depending on the variable values being shown. The model is presented in a perspective projection, and lighting and shading parameters are specified to make the 3-D geometry look as real as possible. Direct trade- offs need to be made between quality of the display surfaces and the timely performance of display updating. After much experimentation, it was decided to maintain a reasonable display quality despite long draw times, based on the assumption that the performance problem could be reduced in the future with the use of a workstation with greater processing power. Manipulation of the 3-D model is provided by valuators on the screen. A valuator consists of a box with a sliding handle whose position can be controlled by dragging the handle with the mouse. The position of the handle corresponds to a particular value of a viewing parameter. One valuator controls the size of the f ield of view, providing for a zooming in/out function. The others control the angular position about the x, y, and z axes of the model in the workstation by changing the view position in the x, y, and 2 directions. The same variable types are available for display as in the 2-D environment (power, effort, flow, energy, momentum, displacement, signal). Data loading, calculation of momentum and displacement values, and scaling functions are also the same. The variation method provided for showing values is color change on each bond. Bond width was not used as a variation technique, since 3-D perspective drawing of the graph causes parts of the model that are further away to be shown smaller than parts of the model at the front. Changing bond widths to represent information would cause erroneous conclusions due to the perspective effect. Ten levels of color are provided based on a 48 VBGYOR (rainbow) type spectrum with violet as the low value and red as the high. Reference bond directions are reversed in the display to show negative variable values. Functionsfor controlling the animation with respect to time are provided which are similar in nature to those of the 2-D environment. Animation at a constant speed and step-type functions are provided within the 3—D framework by choosing buttons in a selector window. Each time the animation is updated the nodes are redrawn in the neutral color, while the bonds are redrawn in the appropriate colors corresponding to the chosen variable value. A key is also provided to index colors with numerical value levels. Currently the BGVis-3D environment can be used for display of 3-D bond graph representations and not for graphical construction of the models. Two-dimensional model files can be changed to three-dimensional model f iles by using a text editor and manually typing in z coordinate values. It is anticipated that a three-dimensional model builder could be constructed using techniques directly corresponding to the current ENPORT two-dimensional model builder. Since the intent of this project was to show the value of enhanced simulation results display, it was decided to leave 3-D model building capabilities to a future time. 4.2.2 Platform Selected for Implementation The implementation of this research was also performed on a Sun Spare-10 workstation running the UNIX operating system. The 3-D display post-processor is implemented as a stand-alone module that can access ENPORT (1.0 8 version) library routines necessary for f ile reading and any other necessary utilities. Three-dimensional models can be loaded from ENPORT model files which have been modified to include a third coordinate. To support this modification, the basic data structure defined in 49 ENPORT to store node and connector data was altered. This also led to modifications to the file reading/writing routines. Documentation and the computer code generated in the course of this phase of the research can be found in Appendix B. An example illustrating the utility of the 3-D display environment can be found in Chapter 5. In order to build a 3D modeling environment with the characteristics described above, it was necessary to either find or build programming software capable of performing the 3-D graphics tasks. The fact that developing computer graphics code for allowing 3-D display of ball and stick type structure is very time consuming and the desire to make portable code led to the use of a graphics standard to support the modeling effort. The PHIGS graphics standard (Kasper and Ams, 1993) was used to supply the capability for controlling and drawing 3-D geometries, including lighting and shading effects. A description of PHIGS can be found in the next section. 4.2.3 Description of the PHIGS Graphics Standard A computer graphics standard is a set of computer graphics subroutines which has been established as a basis for performing computer graphics operations. It has generally been designed to be as portable as possible, allowing the applications using the standard to be used on different computer systems and to be useful in a broad range of graphics application domains. The standard is also designed to be independent of computer programming language used. Several different graphics standards have come into existence since the late 1960’s, when development of standards was begun. Among the first was the Graphical Kernel System (GKS), which was specified to address 2-D display of computer graphics. GKS was also later used to support 3-D display, and GKS-3D was published in 1988 50 (Int’l Standard, GKS-3D, 1988). Another standard was developed and presented around the same time which supports both the modeling and viewing functions of computer graphics. That standard is called the Programmer’s Hierarchical Interactive Graphics System (PHIGS), and this was the standard chosen for use in creating the 3-D bond graph display environment (Int’l Standard, PHIGS, 1988). PHIGS is described as “a set of functions for computer graphics programming in environments requiring rapid modification of graphical data that describes geometrically related objects” (Arnold and Duce, 1990). The 3-D bond graph environment falls under this category of applications and thus the PHIGS standard was considered useful for developing the software. An addition to the original standard called PHIGS PLUS was also defined later to provide higher level capabilities for lighting and shading calculations (Int’l Standard, PHIGS PLUS, 1992). This standard is also used in this work along with PHIGS. Some of the basic characteristics of PHIGS and how it is used in designing graphics applications will be described here. Since PHIGS is defined independently of programming language, it was necessary to use the standard-specified C binding for PHIGS, which defines how the functionality of PHIGS is tied to the C programming language. All programming done in the course of designing the 3-D bond graph environment was written in C. An important feature of PHIGS, and one on which the standard is based, is the concept of a workstation. PHIGS uses this term to mean “an abstract collection of hardware and software with graphics capabilities” (Kasper and Ams, 1993). A particular workstation is implemented by connections to physical output and input devices. There are some functions of PHIGS which are workstation-independent, i.e. designed to be portable between all hardware systems, and some functions which are workstation- dependent. 51 The functionality of PHIGS allows for creation of device-independent graphical models by defining graphical data units called structures. These structures consist of hierarchically arranged element primitives or building blocks along with their attributes. The structures are stored and can be accessed by their application-specified names. Editing of these structures after initial creation is also allowed. Once the graphical model has been constructed, PHIGS provides routines defining the viewing parameters for the model. Finally, the model is posted to a workstation for display. In the course of graphics modeling and viewing, it is necessary for the model to go through a pipeline of coordinate transformations. A diagram of the PHIGS supported modeling transformation pipeline is shown in Figure 8. The initial model is described in a modeling coordinate system, which can be chosen for convenience in constructing individual pieces of a model. A world coordinate system is defined which allows individual pieces to be assembled into a larger model. Thus model subcomponents can be constructed in a local coordinate system and then be scaled, rotated, and translated be before placement in the global modeling space. 52 3-D Elements J Modeling Coordinates (Composite Modeling TransformatioD World Coordinates (View Orientation Transformation) View Reference Coordinates (View Mapping Transformation) Normalized Projection Coordinates C Workstation Transformation l Device Coordinates Display Figure 8. PHIGS Modeling Transformation Pipeline. A view reference coordinate system can be chosen to select the direction from which the model will be viewed. The model in view reference coordinates is then normalized in preparation for display on a particular workstation. The final transformation takes place changing normalized projection coordinates to device coordinates, which are the actual coordinates used to display the model on a particular graphical output device. PHIGS provides routines which support all of the functions described in a way which ensures that the user does not have to deal explicitly with the mathematics, primarily matrix identification and multiplication, involved in the transformations. It thus provides three-dimensional graphical processing capabilities at a relatively high level which can easily be integrated into an application. 53 4.2.4 User's Guide The following section can be used as reference for running the 3-D dynamic display environment. Each of the functions available is described under the appropriate heading. Starting the 3-D Display Module. The 3-D Display Postprocessor can be loaded by typing the name "enport3D". This window provides the functions of loading of model and data files, specifying the time range of the display, selecting the scaling type and variable to display, and opening the PHIGS display window. A picture of the 3-D postprocessor control window is shown in Figure 9. Exiting the 3-D postprocessor can be executed by clicking on the "Quit" button. Wt/I/mmwot-firefl- Figure 9. 3-D Postprocessor Control Window. 54 Loading an Output File. Clicking on the "Load Data” button will bring up the directory structure window which will allow the user to select an ENPORT simulation output file (suffix .S2P) previously generated by the ENPORT solver module. Clicking on the f ile name will then cause that file to be loaded into the 3-D postprocessor. Loading a Model File. Bond graph model data can be loaded into the application using the "Load Model” button in the same way as for the data file. The selection window can be used to select the z-modified ENPORT model file (suffix .ENP) to be loaded. This file contains the system graph as constructed by the ENPORT model build module, but modified to include a third coordinate (z) for all of the model elements. Determination of all output variable ranges occurs at this time. Selecting a Time Interval. The default time limits shown in the initial and final time boxes are taken as the beginning and ending times of the simulation (see Figure 9). If some subset of that time interval is desired for study, new time limits can be entered into the boxes by simply typing them in using the keyboard. Choosing variables for display. The choice for which of the seven variable types (power, effort, flow, energy, momentum, displacement, signal, none) to display for color variation on the 3-D model are made by mouse selection from a pull-down menu provided near the bottom of the control window (see Figure 9). Clicking and holding in the box to the right of the menu label will cause the pull down menu to pop up, and the mouse can be dragged down and released on the appropriate variable option. Choosing a Scaling Method. The program allows three choices for scaling of variables: linear, logarithmic, and absolute logarithmic. The choice of which to use is governed by the pull-down menu obtained when the button next to the "Scaling Type" 55 label is clicked and dragged down to the appropriate choice and then released. If negative values of the chosen variables are present when logarithmic scaling is chosen, an error message will be shown. Entering the 3-D PHIGS Display Module. The model can be displayed by choosing the “ToPhigs” option once the model and data files have been loaded. A PHIGS workstation is opened, and the bond graph is displayed there in three dimensions. The workstation in this case is an X window. A picture of the 3-D display control window is shown in Figure 10 for reference. The graph is displayed with spheres as nodes and rectangular solids with arrows as connectors. The model is presented in a perspective projection and lighting and shading parameters are specified to make the 3-D geometry look as real as possible. Manipulation of the 3-D Model. Manipulation of the 3-D model is provided by valuators on the screen. Four valuators are present. One controls the size of the field of view, providing for a zooming in and out function. The other three control angular position of the model in the workstation — one each providing rotation about the x, y, and z axes respectively. Each of these valuators can be worked by dragging the button to different positions along the track. Controlling the Animation. The controls for running the 3-D animation are included in a selector window popped up along with the valuators by the PHIGS workstation. The same buttons are provided as in the 2-D environment See section 3.2.3 for details of how they work. 56 Interpreting the Data Key. A smaller workstation is provided to show the numerical scale values of the displayed variables that correspond to each displayed color. The current time stage value is also displayed at the bottom of this window. Leaving the 3-D Dynamic Display Module. Click on the "Exit“ button in the selector menu area at the far left to close the window and exit the dynamic display control window. The entire program can be exited from the higher level window. 'K.““-!"- g ..,.. ', 0.“ At, a °' k .3“ I.” ","z 0 .. .1 :‘ A. ‘.i 4 9 1 ‘7 a,» - g-..“ fi 6 Figure 10. The 3-D Postprocessor Display Window. Chapter 5 Visualization Examples Using BGVis-ZD 5.1 Automobile Modeling Example In the field of automotive engineering one of the critical tasks is to design automobile suspensions for good performance, for example to provide reasonable settling times and limited motions for the car chassis and passenger due to a displacement disturbance from a rough road. As an example to demonstrate the capabilities of the two- dimensional bond graph visualization tool (BGVis-2D), the three-dimensional vehicle illustrated in Figure 11 was chosen for study. This particular example was chosen for two reasons. First, because the vehicle is a real life engineering system design problem. Second, because the system is straightforward enough for exPerienced engineers to form a conception of how the system will perform under different inputs. The purpose of the BGVis-2D environment is to provide insight into the behavior of an engineering system. The benefits of using BGVis-2D are clearly demonstrated by comparing the visualized response against the expected response. A schematic diagram of the car chassis unit and suspensions with seat/passenger is shown in Figure 12. The schematic model functions as follows. The car chassis unit is treated as a rigid body which is allowed to translate (bounce), in the vertical direction (2 axis), and rotate about the Y (pitch) axis and the X (roll) axis. For simplicity the angular motions are assumed to be small. An independent mechanical suspension system is attached at each comer of this rigid body. The comers thus experience different vertical (Z-axis) displacements depending on the position and orientation of the chassis. The 57 58 suspensions consist of a spring and damper connected in parallel to the axle. A wheel is mounted to each axle and maintains contact with the ground. The input to the system is a vertical velocity applied to each wheel induced by the car traveling over a specified ground profile at a constant linear speed in the horizontal direction (X axis). A seat/driver are included in the model, connected through a compliance and damping effect to a point in the front half of the chassis. One of the primary responses of interest is the position of the seat/passenger in the car, which is allowed to vary in the Z (vertical) direction. The following section will consider a three degree-of-freedom bounce/pitch/roll (BPR) model of the vehicle dynamics. A two-dimensional bond graph representation will be used. A three-dimensional bond graph representation of the BPR model is described in chapter 7. Figure 11. Vehicle System Illustration. 59 Y q (Pitch) Seat and pmsenger Figure 12. Schematic of Car Chassis Unit and Suspensions with Seat. Bond Graph Model Description. The BPR model of the vehicle can be thought of as consisting of several major sections, or macros, which are connected by power bonds. Figure 13 shows the macro bond graph of the BPR car model. The seat unit is connected to the rigid chassis unit by a rigid connection labeled CS on the graph. Each of the suspensions is connected to a comer of the car via a rigid connection. RF stands for the right front comer, LF for left front, and RR and LR for the right and left rear comers, respectively. Each of the suspensions also maintains contact with the ground. Viewing the model as a macro bond graph representation is very useful if overall system response is of concern, rather than individual responses occurring within each subcomponent. A macro construction feature is currently not available in the workstation version of 60 ENPORT, but it is intended as an addition to the functionality of the program in the near future. Adding macro viewing capability to the BGVis-2D tool would assist in assessing the behavior of systems, especially in very complex systems with large numbers of bonds. [ ) 1C3 C Rigid Chassis Unit .1 .4 .. Suspension Suspension Suspension Suspension Unit 1 Unit 2 Unit 3 Unit 4 RFG1 1 RRG1 LRG LFG Figure 13. Macro Bond Graph of BPR Model. For the purpose of simulating the behavior of the BPR model, each of the macros was expanded in detail using basic bond graph elements. The bond graph representations of the seat unit, rigid chassis unit, and suspension unit will each be shown and explained. The 2-D bond graph representation of the seat unit is shown in Figure 14. Node 126 represents the vertical motion of the seat unit. The SE6 node includes the input force on the seat due to gravity and the 1M6 node includes the inertia effect of the seat unit mass. 61 RD and CK are the dissipation and compliance effects of the coupling between the seat and the point on the rigid body chassis to which it is attached. SE6 -—>- 125—4- 1M6 / OZ—> 1D \ CS CK Figure 14. 2-D Bond Graph Representation of Seat Unit The rigid chassis unit bond graph model is shown in Figure 15. The TF nodes and their connectors represent the geometric constraints satisfied by the rigid body. The 1W junction represents the translational motion of the rigid body chassis in the Z direction, while IP is the roll motion (about the X axis), and IQ is the pitch motion (about the Y axis). The 0218 junction serves to calculate the position of the point on the rigid chassis to which the seat unit is attached. 0217, 0211, 0215, and 0213 each determine the position of a corner of the rigid chassis to which a suspension is attached. All velocities and forces are considered positive in the downward direction. All rotational quantities are taken positive in the directions indicated on the schematic of Figure 12. 62 TF8 TF7 \‘m \ “:17 \ <~ TF1 1v TF13 7 TF17Y {» TFISY l /rF13Y / 0217 Ole 0215 0213 A A ml ml Figure 15. 2-D Bond Graph Representation of Rigid Chassis Unit. A detailed schematic of one of the independent suspension, axle, and wheel systems which attaches to a comer of the chassis is shown in Figure 16 along with the corresponding bond graph. The stiffness and damping of each suspension are represented in this model with mechanical elements (CSI and RS1), but for an industrial application the suspension unit could be modeled as an electronic active suspension containing electrical and hydraulic components as well as mechanical elements. With bond connections between the suspension elements at different corners of the car, non- independent suspensions like roll bars also could be modeled and analyzed. The axles and wheels are modeled in this example with inertia (1W1), resistance (RWI), and compliance (CW1) effects. The schematic shows the coordinate systems used to construct the bond graph. 63 Attached to car body at comer r ; Vcar 1217 RS 1 Suspension \ / axle Maxie Vaxle l SEWl / RWl Wheel ‘\ 1W1 v- 01 _ CW / d l RFG groun } Vground (a) Schematic Diagram (b) Word Bond Graph Figure 16. Detail of Single Suspension Assembly A two-dimensional bond graph of the entire three degree-of—freedom BPR vehicle model is shown in Figure 17. This model is formed by joining the sections described previously, connected as they were in the macro bond graph of Figure 13. One simplification was made in the full model, which eliminated the 12 node of the seat unit. Each vertical branch in the full BPR model bond graph represents a suspension and wheel series. Branch 1 is the f ront/ri ght suspension, branch 2 is the f ront/lef t, while branches 3 and 4 are the rear/right and rear/left respectively (corresponding to the schematic in Figure 12). The ground connections are represented by source of flow nodes. A vertical velocity is imposed on the wheel which is induced by the interaction of the forward 64 horizontal velocity (assumed to be constant) and the shape of the ground position profile that each wheel experiences. More details on the velocity input modeling can be found in the next section. Table 2 contains a summary of the equations used for this model along with their parameter values. S56 —" 126——. N6 l m seat unit IOZIN \ i I 5/ z! _. > 4 TF” . TFllY 11:15}. TF13 11:13} 1 WHY I ngrd 2 / . chassis / i g m. 0217 02411 0.2115 0213 RS] 1317 R82\ 1311 12F RS3 1213 RS4 117‘017 111l—-011 015-5115 013-3113 CS4 CS” . 1 s 1 l ,. \z. \‘ cs2 - 1W1 1W2 [W4 1216 l/ 1210 1214\ Mac8 1le ...—> sgw/ sr—zwz SEW3 \SEW4 112w RW3 RW4 ' /1wr‘-RW012\1W21—02 CW1 C“r2 CW3 CVV4 : 1 5121 s14: Figure 17. Two-Dimensional Bond Graph of Car Model. 65 Table 2. Car Body and Suspension Model Equations and Parameters C unctton e W a .— II II II 1 t ("H nllll r-o l 33 I t I I "He-o "1111 0". F00" II II H II pus II 11 BB System Response and Assessment. The bond graph model of the car body and suspensions was subjected to an input consisting of an encounter with a relatively large pothole in the road. The pothole was modeled as a function following a sinusoidal profile. The vertical velocity induced by this function was determined and applied to the right front tire at the time the pothole was encountered. The same velocity function is experienced by the rear tire, but after a time delay which is dependent on the horizontal velocity of the automobile (for this example, approximately 35 mph). Figure 18 illustrates the mathematical modeling of the bump input. The ENPORT model file and function definitions for this example are included in Appendix C, along with the initial conditions used for the simulation. 0'150 0.1 0.2 03 0.4 0.5 _ 0.6 x distance (m) Pothole Profile: 2 = ~0.075*cos((10/3)*Pl*x) +0.075 for 0 < 2 < 0.6 Vx = 13.42 m/s V2 2 dz/dt = dz/dx * dx/dt = dzjdx * Vx t: x/Vx '1’0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04 0.045 time (5) Vertical Flow Source: V2 : (3.355)*PI*sin((10/3)*PI*13.42*t) Time delay for back wheel: t = length of car/Vx = (2.5 m) / (13.42 m/s) = 0.19 s Figure 18. Mathematical Model of Pothole Source of Flow. 67 Table 3 shows a tabulation of the response values for the suspension spring deflections of the system (Q42, Q45, Q48, Q51) to the pothole input over a time range of 0.5 second. This response was obtained by setting the initial values for the displacements to their equilibrium values (see Appendix C) and solving for the response using the Runge-Kutta integration routine in ENPORT. It is obvious that this presentation of response as a table of data is difficult to interpret in terms of the geometry of the model. Figure 19 shows a time plot of the variables mentioned above, along with the position of the seat and passenger with respect to the chassis (Q86) for the same 0.5 second time period. It also takes considerable effort to relate this presentation of variable values back to the bond graph and the schematic, and to visualize their meaning. TIME +0.00000E+OO +2.00000E-02 +4.00000E—02 +6.00000E-02 +8.00000E¢02 +1.00000E-Ol +1.20000E-Ol +1.4000OE-Ol +1.6000OE-01 +1.800003-Ol +1.999908-Ol +2.19990E-Ol +2.3999OE-Ol +2.5999OE-Ol +2.79990E-01 +2.9999OE-Ol +3.20000E-Ol +3.4000OE-Ol +3.6000OE-Ol +3.800lOE-Ol +4.00010E-01 +4.20010E-01 +4.40020E-01 +4.60020E-01 +4.80020E-Ol +5.0003OE-Ol Table 3. Response Data from Pothole Simulation. .32700E-02 .327OOE-O2 .327003-02 .327008-02 .327OOE-02 .32700E-02 .83600E-02 .18300E-02 .06320E-Ol .15300E-02 .49200E-02 .O8lOOE-02 .73500E-02 .503OOE-02 .424OOE-02 .286OOE-02 .23800E-02 .086008-02 .29300E-02 .843003-02 .936008-02 .520008-02 .484008-02 .354008-02 .222003-02 .180003-02 .75100E-02 .7SlOOE-02 .75100E-02 .75100E-02 .751003-02 .75100E-02 .6S3OOE-02 .63000E-02 .llSOOE—OZ .96200E-02 .BOlOOE-OZ .329OOE-02 .37000E—02 .33800E-02 .SOSOOE-OZ .534OOE-02 .79700E-02 .953008-02 .OSlOOE-OZ .239008-02 .319003-02 .l6800E-02 .42800E-02 .49500E-02 .SSSOOE-OZ .673005-02 .95000E-02 .94900E-02 .95000E-02 .95000E-02 .950003-02 .950003-02 .424008-02 .52400E-02 .99100E-02 .lOZOOE-OZ .l69OOE-02 .48000E-02 .293003-02 .24500E-02 .OSSOOE-OZ .24SOOE-02 .826OOE-02 .1834OE-Ol .651003-02 .98400E-02 .253003-02 .329003-02 .Ol7OOE-02 .91200E-02 .85800E—02 .77300E-02 .37200E-02 .372003-02 .372003-02 .37200E-02 .372003-02 .37200E-02 .498003-02 .29700E-02 .58100E-02 .122003-02 .34800E-02 .7SlOOE—02 .90300E-02 .09600E-02 .lZZOOE-OZ .238OOE-02 .70lOOE-02 .624003-02 .30800E-02 .O4SOOE-02 .44lOOE-02 .O4900E-02 .93SOOE-02 .O64OOE-02 .199003-02 .26lOOE-02 ErgonI/u_sr.o-oeta 11:11:54 09/13/94 § " ' 1{ ' ‘ . 2*.\ i w /Ii\M fi 3 a: '2 r' . ;‘<:;“I; . '. . ,' . . -~.___ , . . 2 :3; : I -' . ' . ' g . I . 4 v . - Hz ‘ '. 1 . i 1 ' ., (.1 l : . , Figure 19. Response Data from Pothole Simulation Response Using the BGVis-ZD Tool. Several figures are shown to illustrate the assessment of response of the BPR vehicle model to the pothole using the enhanced bond graph display environment The variable type selected for line width display in these figures is power. The first (Figure 20) shows the car at its equilibrium position before the bump is encountered. Since at this equilibrium point the parts of the vehicle are not undergoing any vertical velocity, powers are all equal to zero and all of the bonds are drawn at their minimum width. Figure 21 shows the response of the system at the time just after the front/right tire has encountered the pothole. Power can be seen to be flowing up branch 1 (right/front) into the CW1 element as the tire responds to the downward velocity. In Figure 22, power flows further up the suspension branch to be dissipated by the suspension's viscous damping (RSI). F1 gure 23 shows that the power 69 input to the model by the pothole is nearly damped out by this damping effect at a later time stage. In Figures 24 through 26, responses are shown at a time after the rear/right tire has encountered the pothole. The response follows the same pattern as occurred in Figures 21 through 23, but now power can be seen to be transmitted up branch 3. The line width variation technique lends itself well to the visualization of ”flow” type quantities within the system. In addition, Figure 27 shows a display of energy variable values using the "level" indicators at a time soon after the front tire encountering the pothole. The glyph symbols next to the R, C, and 1 elements indicate that at this particular moment in the course of the animation energy is stored kinetically in the I element for the wheel/axle (1W1), while a small amount of energy has been dissipated in the suspension (RSI). Eventually, the majority of the energy input to the system by the pothole is clamped out through the action of the R elements in suspensions 1 and 3. The "flow" and "level" type indicators could also be used together to enhance the engineer's understanding of how the system functions. For the purpose of checking exactly how much relative displacement is experienced by the seat unit during the simulation, bond 88 was selected with the mouse, and the time plot of displacement shown in Figure 28 was obtained. The time plot shows a small change in the absolute position of the seat unit mass during the course of the simulation for the chosen model parameter values. It can be concluded that although less than one tenth of the maximum power transmitted to the wheel ever reaches the car chassis and passenger (as shown by Figures 20 through 26), there is still a small amount of deflection experienced by the passenger. These visualization techniques give a qualitative idea of how the vehicle reacts to a pothole in the road, which would allow tuning of the suspensions to further isolate the road surface from the passenger motion. 7O oomo . O ........................... I Q! 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'l' 1 I 1" I. I ....fi.................,... 4.3.7.3:.-.:.:.~.-.-.:.'._-._-.-.j.- j 34.-4.3.: / — .. Xxx. H MBH Illrwémd Bo; vmu \MnO Mmu SQ \s\. \ZVOV 0' Mfiu MdNu mu— om w on; C. vmm MHNO Mmm \/ Km; 0. 0h \ a w... OaNa IIV NEH 53. z~o~\_ WHO "HO Nmu /// :3» 5.8 mv/,/ 5. ,r mdNu adNfi and vac no; 3‘ \mLNO/AaaNO Nmm -. /.. ..\ MHH/ / ...“... , . «MAE: W... \ Wlmafla 3:. a; /../s We“ 33 Em m3 Em Sm D: Em :8 ~1— \ 1‘ Ex win 3.: :3. max All mine 52 mixillv NE: 3 - / \ w \ 0 Sam 3 «5 Sum mo fl mim a» :35 V \1 ...... QHNA llilv "EH zmfiv to 3b 4. /. xv..." 0v .// No. .r. F: m 3 ~- w 3 w 5N: 7mm ....» a 1.. >~auk .Ilnlwlth—LP- Usuallmm / A: RA~3\\\ 3L9: .. 8 z , . . . am‘ t» .a, 3 (lift! 8 x \. ll y . a “I,“ \ xullllkofialllibmm m—ro am 3 : ozmdlllku o... .flfllll 0mm Figure 25. Power Variable Response for BPR Model (Time = 0.305). 76 ............. ........................... ............. WW“? .'.‘-' n'u'.'- nay-.0144: . . .' _.'.‘,'._ {lififi'WE-Y’FI‘Y-f-Téfififif‘ffir‘.‘ A.X......yiffisafifiacfiéific<§x¢$c .u.u.u¢...u.m.u.m ”+2 . k8. .. 4 ogsfisuiosxgfififi VBU cum MBUMn—m Num 9...”. Hum 2.: Sr. av ...... ma— V3m «Ml V3" 50v MEN. Ill Wagon Sow N13 IIIIV N313 "3" llilllV “Em ¢ / D N 07 a \d a\ V3mm VO MBMW M0 N0 \Nme w 4 .\ M- S R «~ 8 \R\ Z VBHAIIIINHNH MBHIII'VnNd OHNHflvlmIINBH ®~Nn|~n|V~3H on on floor. :98. z~o~< x33 vmu MHO MWU mac «"0 Nmu mwo «mu \ x/ / i . X/ . nm# \: xvov 0' 2'0" IVGN nv ;. wv 21c“ I “1 Sam ,A 3 /,r m: Maw" m: mama “am“ a: ham“ r. «v muwo n a H [ring—a m d4llmm 0v: ISIIV 0N" iwolllv mum. ..... . . . . I u. ‘- .. n .- .. ............................... ......2. ............ s >............u.u..u.u.u.. namingtit..93....”.3 Antananun ”...”.u ...”...Hmfimr3...... . animaawuuwnna.”.u......uufihu.r.nv ......... A... ................................... 0.325). Figure 26. Power Variable Response for BPR Model (Time ommfid '1 E '1 p,— ii 0. r m 4444* ‘3‘. 124 El 3 kl O N I" R O N .3 .4' .1 .3 «I «I E2Ilgl . . in '§ 0 a R n' :35 Em szumum m E .2 3 SEE pl: 2: :2 2E Illa 3.5 a.“ 7/ 7, ...x Kim 3 «.0 Dim . mo 8.. Dim. 7. , ,. . n: mare we L Dov: lowlv 0N." Aool mum .3. m ,2 3.: . :E :_m_u Figure 27. Glyph Display of Energy Response for BPR Model (Time = 0.135). llllllllll ng Q88. [1 ed by Selec Figure 28. Time Plot of Displacement Obtain 79 5.2 Rallcar Air Brake Switching System Example The DB-6O Control Valve is part of a power braking system used to stop railway train cars. The braking system consists of pressurized air brakes which provide friction to the wheels of each car to decrease its speed, a brake pipe containing pressurized air which extends from the engine to all of the cars, and the DB-6O control valve which directs air to the air brakes from storage reservoirs as necessary depending on the engineer’s control of brake pipe pressure. The storage tanks are also included in the system, and the switch controls air flow to these reservoirs for charging and recharging of the system as well. The DB-60 is a combination of hydraulic and mechanical components. Figure 29 presents the schematic diagram of the railcar airbrake control valve given in the DB-6O Control Valve Instruction Manual ME—21 (New York Air Brake, 1991). The manual consists of thirteen three-page-wide color plates and twenty-eight pages of explanatory text all for the purpose of educating an engineer about how the system functions. The air brake control valve was chosen as an example for this research because it is a complex, industrial level modeling problem involving moving mechanical parts and pneumatic circuitry, and therefore illustrates the necessity and effectiveness of better visualization. The BGVis-ZD tool is of great value in supporting the construction and verification of a working model of the air brake system. A model which has been validated against actual test results would be a very useful tool for testing proposed design improvements. Model Description. The construction of a bond graph model for a system as complex as the control valve is not an easy task. The approach taken was to hierarchically decompose the overall system into successively smaller and more detailed subcomponents and their connections. The key activity involved in this modeling decomposition is the identification of the ports (input/outputs) of the system as a whole .02; Gli- 22335083 2..- .o::oo 00 no 11111 1.! ..ch 98:33 I; £615 faves}: :2 If: III-1 frilly Ila-u ruli- Figure 29. Schematic of the Air Brake Control Valve Switch. 81 Figure 30. Top Level Bond Graph Decomposition. and of each individual sub-system. The result of the first step of identifying the input and output ports from the environment to the DB-60 device being modeled is shown in Figure 30. This figure also shows the breakdown of the main device into subdevices called the DB-lO Service Portion, DB-20 Emergency Portion, and DB-30 Pipe Bracket modules. This example focuses on the 03-10 module. The reticulation of the DB-lO module into seven subcomponents, following the numbering convention established in the Instruction Manual, is shown in Figure 31. The pneumatic ports from the environment to the DB-lO unit are the Brake Pipe (connector BPl), the Emergency Reservoir (connector ERl), the Auxiliary Reservoir (connector (ARI), the Brake Cylinder (connector BCl), and the Retainer (RETl). Connectors RP and E? are ports to the atmosphere and RVH is a mechanical port. The figure shows sub-devices numbered 82 0 through 6 and their interconnections. Due to the complexity of the system, only those subdevices necessary to the functioning of the different modes of operation under study in this example were modeled. These are described in the following paragraphs. "III I!» 9 Figure 31. Bond Graph Decomposition of DB-lO Module. Modes of operation. The DB-lO module is designed to perform many different functions depending on brake pipe (BP) pressure and pressure levels in the storage reservoirs. Several have been identified for modeling. When the storage reservoirs are empty, an increase in BP pressure causes charging of the auxiliary reservoir (AR) and emergency reservoir (ER) from the BP. Charging involves primarily the Service Main Piston System (1) (see Figure 29). In a standard braking procedure, a decrease in BP pressure causes air from the AR to be directed to the brake cylinder (BC) to stop the train. Standard braking also primarily involves the Service Main Piston. After braking is completed, BC air is exhausted to end brake application, and ER air may be fed into the 83 B? to support recharge of the system. Recharging occurs with assistance from the Service Accelerated Release Valve (2) as well as the Main Piston. At any time, a manual lever can be used to exhaust the AR and ER to the atmosphere. Manual release involves the Release Valve (6) in combination with the Main Piston. These subdevices of the model were modeled appropriately and correctly connected to each other. Equations were set up for each of the elements using reasonably estimated parameters. With the parameters set, simulations of the different modes of behavior of the device were completed. Before presenting the entire system model, a modeling and simulation exercise involving the Service Accelerated Release Valve (2) will first be described. The behavior of this subsystem is also visualized before moving on to the full Air Brake Valve System model. Check Valve Modeling. To verify the concepts involved in creating bond graph models of pneumatic/mechanical devices. especially modeling of check valve (CV) behavior, a bond graph model of the Service Accelerated Release Valve (2) only was created. A detailed schematic of the subcomponent is shown in Figure 32. The bond graph model for this device is shown in Figure 33. The device consists of a Back Flow Check Valve (2-1) and a diaphragm actuated valve (2-2) which together control flow from the emergency reservoir to the brake pipe. Figure 32. Schematic of the Service Accelerated Release Valve (2). C5021 CstZl ‘\ 211cm 1c» \ , c5022 Cst22 \ / \ 7 121 v—gi—I— 1X21 __fl.> 921 Vic”: [(21:30, I 21551 2211 ‘\ / 2219 122 - 1>:22 ——» R22 I SE21 22m A 21035 TF22 I 21091 0R21———> Rx21 221” I ‘ - as: 22 ‘1“ Ccomp 539R - 1 18P22 RxZZ I E912 SEER —————\ IBPZI 060w l221R>; m l - o in- _ Ucomp 1 ABBA—‘9 " 1ER22 [22510 392 22 4" SEBP 1 ‘ OBP22 Figure 33. Bond Graph of the Service Accelerated Release Valve. The CV is modeled as a mass which is allowed to translate in the X direction (1X21). Forces on this mass which affect its motion are l) the force due to the spring (Csp21); 2) a force due to the stop when it is encountered by the mass (Cst21); 3) a force due to viscous friction (R21); 4) an inertia force (121); (5) and a force due to the differing pressures on each side of the mass (through bond ZlSEl ). When the displacement of the CV is positive, and the pressure difference over the CV is positive, there will be flow through the valve (from SEER to 0comp) which can be calculated by a non-linear relationship depending on the values of the pressure difference and the valve opening dimension. This equation is implemented by the Rx21 node. The diaphragm actuated valve works in the same manner, where flow from 0comp to SEBP is only allowed if the pressure difference over the diaphragm overcomes the spring force causing the valve to 85 open. Therefore, in order for flow to occur from the ER through to the BP, the AR pressure must be lower than the BP (to open the diaphragm actuated valve), and the BP pressure must be lower than the ER pressure (to open the check valve). This sub- component thus provides ER air to the BP for recharging when the AR pressure is low, for example after a standard braking application. A simulation of the Service Accelerated Release Valve has been performed to verify the basic behavior of the model. Parameters were estimated to achieve reasonable results. Details of the parameters and equations used for the bond graph elements shown in Figure 33 can be found in Appendix C. Verification of the expected functioning of the component can be easily seen by using the BGVis-2D display of the power variable type on the bond graph using line width variation. Figures 34 and 35 show two different time stages during the course of the animation. In Figure 34, at time = 0.5 it can be clearly seen that no power transfer is occurring in the device (minimum line widths for all bonds), since the AR pressure is low, but BP and ER pressures are equal. Figure 35 is used to illustrate the use of color as well as line width variation by the BGVis-2D tool. In Figure 35, at time = 0.76, the AR pressure is still low, and the BP pressure has experienced a smaller decrease. Color variation on the bonds shows pressure on bond ER12 is greater than pressure on bond BP2122 which is greater than pressure on bond AR2122. The line widths show that there is power flow through the valve (large widths for bonds all along the path from SEBP to SEER). The arrow directions indicate the direction of flow. Thus the model behaves as intended. In addition, Figures 36 and 37 show the flow variable type displayed with line width. At time t = 0.21 seconds, the AR pressure is decreasing, causing the diaphragm to move. This velocity is shown by the large line widths connected to the 1x22 node in Figure 36. At time t = 0.6 seconds (Figure 37), the BP pressure is decreasing. This 86 causes the check valve to move into the open position (larger bond widths on the 1x21 node), while the diaphragm (1x22) moves back somewhat toward its initial position since the pressure difference between AR and BP has decreased. Arrow direction changes on the bonds connected to node 1x22 show the occurrence of negative flow. The visualization provides a qualitative analysis of what is going on in the device without having to select individual bond values for display of time plots. Rextuamn. fiagdt lute...“ dwflwnfivfiwfigwngwfiufikmo .u....n.....u.n.n.....u... u.n.....u.”.n.u.u.u.u.“.3.”$3.30 .... mmmmoi 38.8 ammm QEOU NNmm: [lg 33 O 4/1! 30“ /’t/Ifl gnaw precuo “mama dilummll Mumm ‘ -..... -llll l, V . LEO. 6»fo CCLCfi NWuNS mcmm L .... 7.. < .i q... Ill. lul: a ... firm dc n. :88 cm- 1.9.. NNLH WMCdN , Notumud {Em 73m .................. .............. , rare-5:25.54 ‘ NNmmmullNNXa :NN lV NNH «um«~ :-3¢:'1‘2':"-52-:- 1135':- 283 183... E a .r/ ..x. . , 2.x... mmumu mmam u / . / yawn auUSN ,. .2 Emumw fimauu 1' H (\J (I l \ o—d (\l x ‘ ,/ v—c H (‘J H :lrifvéfififi: '2".CjI'Z'IWCWfipfifigkifififiifififfifirxfiyi-Z :-:-r'-:i:l:-:1:§:i:i Figure 34. Power Variable Display for Check Valve (Time = 0.5). Halalkl: I. l“ ~00~<~1v¢v¢~4~ Isl? 5 ’5. '9’ g E ‘5— dnmmn *iwun oudN (Nxz indelFl AND-O onu««~ toad!“ 0.76). Figure 35. Power and Effort Variable Display for Check Valve (Time Nmmmo I 28% ammm on QEOU NNEH: lg 38 O Ali/fir: amen Jill.-.) . . xaamm £000 duLmH llMHQIullll mmwv ‘ a Du v E NNxm Nmmmu 283 acmm u 23 v uh- "Nxm 4H.M«l~l ammo . , Nun: wmoam oodmd n ma: 4 EN; «EN «mum m._._.M.M.U._._._.H..... he. .. 5. «0.3...» m Nwmi NNX iNNH 3mm. «Yuk; w 3.8.8.8! I . < test... Lords N :3 .55 Em lien 81 :3 RH ~?u~a.~ \ / i I / "OIUOhod aw .\ III 4mg.“ NNH U NN U $3 Lau««~/,,/ i I \ 1,9 ......sl... n38 o “New”. Rama n00uo~.v I l 8.30.0 g 0.21). Figure 36. Flow Variable Display for Check Valve (Time “ifi$$3§$$¥fi%3¥.3r¥:",AJuiu: . , ..,.:.7.‘,-.:.3._.:.- . . '.'.:.,_. ,. \Sran in)... 1251..)- \“a .1.- ¢«- anumu‘\\‘_uuuuuulllliv Nmumu Nmumu wflw» ..... yum Ewan amfimmfifil vx 2,?nnuu:u”3...“....Hmmmhwfimm.WHEN.» .. Nmmmo -a~nl I Qmmm owwww~\\\\\mw NNmufi A Aommmw .83 aeouo x¢fi- etcouo mwxm mmmma A was mqmm 988 uhfiwu Nmuh «u»- NNm 1 wafi 4 NNH l/lul tar; . - , . “raw: A|M-Eu-.lll, alga cgm «maul- r illl Hump. .aoam wacaN fiwmm ammu~ «Natl-null- fimxfi '3'" “NH SNN Hmauu Figure 37. Flow Variable Display for Check Valve (Time = 0.6). 91 Main Piston Modeling. With regard to the overall air brake control valve modeling task, the objective was to model the modes of behavior of the device described previously using ENPORT. The modes of operation that were simulated and visualized in this example were: 1) initial charging of the auxiliary and emergency reservoirs, 2) standard braking where air from the auxiliary reservoir is directed to the brake cylinder, 3) secondary recharging where brake cylinder pressure is released and air from the emergency reservoir is directed to the brake pipe, and 4) manual release of auxiliary and emergency reservoir pressure. A bond graph of the parts of the Main Piston System (1), Service Accelerated Release Valve (2), and the Manual Release Valve (6), which are involved in the modes of operation of the device described previously is shown in Figure 38. This bond graph models the ER and the AR each as a C type storage element (car and eer). The 3? pressure is the input to the system (sebp). The velocity of the diaphragm of the main piston is represented as node hr. The forces on the node include a spring, seat, viscous damping, and inertia as in the previous check valve example. Also included is a force generated when the diaphragm comes in Contact with the ER charging valve stem (1x3), a force generated when the diaphragm comes in contact with the AR charging valve stem (1x2), and a force generated in the opposite direction when the diaphragm comes in contact with the BC inlet valve (1x5). The hydraulic flow rate through these valves is determined from the valve opening dimension in elements rx, rx2 and rx5 respectively. The pressure difference across the diaphragm is calculated at node ltf and the force on the diaphragm is determined by multiplying the pressure difference by the diaphragm area at the tf node. The 0bp node is the pressure above the diaphragm, while the Oar node is the pressure below the diaphragm. These areas are connected through several valve and choke pathways to the reservoirs and input pressures. The ER Charging Check Valve is part of the Main Piston sub-assembly and is included with node 1x4 and associated nodes as shown in the box on the graph. The Service Accelerated Release Valve is included at the top of the bond graph with appropriate connections to 92 reservoirs and inputs. The Manual Release sub-component is modeled by the lrel junction. A mechanical force can be input to this element via the serel node, and the position of the release valve controls the volume flow rate through the rxar and rxer elements. Service Accelerated fierease Valve (2 ) csmv 1m) apzl ap22 \\ 1m...)- cst22 m/1 \ ,2, m/ 4 \m «22 ”21 anp rx22 1 valv— omx—r —-¥ amp-Area —-¥ 0bp2 —>1 Abp /., /b92 ~ "'3 ff "*2 Brake Cylmderlnlet Valve (1) m‘ “22"“ {MN \ l' 7 Dw'vaswc’n'xmea’WU) ManualRelemt6) ERCharxmeheckValvem Figure 38. Bond Graph of the Main Piston System and Reservoirs. 93 Made 1: Initial Charging of the Reservoirs. The results of the simulations of the four modes were visualized using the BGVis-2D tool in order to show how the tool helps in making the behavior of the system easier to comprehend. The first mode is initial charging of the AR and ER from the BP. Charging of the system is accomplished by a linear increase in BP pressure supplied as an input. When the BP pressure is increased, it is expected that the pressure in the storage reservoirs will also experience an increase in pressure due to flow of air from the BP through the main piston system. Figures 39 through 42 show this response. Power is shown as a variable type using line width. At time = 0, there is no flow, and all initial pressures are set to zero. Initial displacements for all of the mechanical valves are set to their equilibrium values (see Appendix C). In Figure 39, the pressure in the BP has increased, which causes flow to start through the main piston, which causes the pressure in the AR to increase. Figure 40 shows the system at a later time where the BP pressure has become high enough to start flow into the ER. Figure 41 shows the response as the BP pressure nears its maximum. Air is still flowing into both tanks and power is higher due to the higher pressures and flow rates involved. Figure 42 shows the response after the brake pipe has reached its maximum pressure level, and is now remaining steady. Since there is less pressure difference across the diaphragm, flow into the reservoirs decreases. Eventually all pressures are equal, so all check valves are closed and no more How in the sub-assembly occurs. The manual calls this situation charging lap position. e. A «a HEW“ fifigafiww . ”ya-— a... . v...» ammuunu ..tu...v.ev-... III-E}. ...muxWMfi. ”fix.“ \ 2 «Duo 32 In! v. Lumu do... on ._ M... m. N« Namu Nx... vamxwwmmLe/v; .63. L TEA—AD 795m tn 37 '0‘» $07 mumu N; 3:5” II .500 two .lv 3:. .63 A - \ . 2 2 awn?N x x m 3&3 m an; « MAHIISIIVN... NM cm mm“ .3 umolmmili/Epmmw mmau Al. nuo uo Ill! mnu Lao L3 3 3 .5 lllv ummg K R cw a I/MS a mow we / .50 03 i emu .. N \. 3 B umu XLHIIIIXL .micfllmmu / nn fin // vow dd I LMinImIXH qluuqollkWH an v.0... l/r/ no“ 03 «3.3 / / /. awu mo 2 a 3 .3 III! two lllllv ..mo .3 \\V e mi. n t\-- 3v mmau % moo \tx my... All met; new om / 3.3.“......unnnna. ma fl mXH II, mummy Q20 8 Ugo I'll-L UDU . 3\\ /8 3 ..xn....w.9x...p.2 vn n :33! mL mummy «QDOHI 000... ......e..... man: a 8.5 All .mxe 5.3.3:... / ./ i 00 GO NLU\QA an aflwxaem ! mm mm: mm. s 95 8. 8% L/ 8v \ 2 {v \M\NL ......III mmumumlallmmx Ivmmnmo NNXL Hmumollll. fimxdlilllv Hmwmu I Figure 39. Power Response for Air Brake Model Charging Mode (Time = 18.9). 95 ooom . «m ................u........... 2.35.93.033 538.: I i i i I i i '.‘/.'.'.‘ :-:»:-:-:-: ‘a‘r‘fv‘f-fir 14+ . . . ::.::~.s..:;5rs:~:z:x;<::::¢::azis:z<.. wx Hm ..w ”...R mm» .U”. .f .fi Um“) . A354}: , ..r We Mm, wow. ...mw».m.. €55,352 ..... ....fi flwmuzsamwr vquAlvalilv" a (Emu 7w: 9 v 7 Q . Q “V mv v 7 v3 - 3\ - - ML 2 Nfl N mu Nye v m mem 7; ...mxgil Tue Al TwLau s.‘ .d #7 «39 \ \\ 3A, Mumu , «m I4\«|IVNL er; oIn'Lmuo LLmOIIVvye _. me Lamb filmml o m. \ Dflo\ Jv . «V x \ MQmQKIIrm: mlelv mumwn Lmuu on a. mmfi llnmlderivumolmflmllvsummw ONT mm? \. «Ch mmau~ Ir moo uo AIKII moo .56 gm; :3 .V. \: IJIV pom: O x / / ._ \ fr. 9 - - m3 Lu... W» V L I] R vm :/ . r\ \w nC 2 R xx \ n umu 7 x: ML x; mini/f1 \ gm i Laval- mg I r— d S / L lequuqliuuH , rod oi no? meu 41. moo lillll 75... Ill ,_mu m;& 4.! my}:— MOT «I G9/P ma Moll mxa walv mamu . one lflmllv LLL » mL V0 mva HQDOIQDWU « NQDHMflINQDO \\ 14 AVHNLOIJmILruwa “7 2 /; max. wm NLwWfi on ELM » p... NNL Nqu NNH mm QEU Huawmmm .VfimL 7////,8¢ WM\V -MXA a W\\ mmuwo mum] mmx owl mmamu mmxg Homo [tuba Tm L $1-9 Npmu Brake Model Charging Mode (Time = 58.2). 1!" Power Response for A Figure 4". 98 Standard braking. The main piston system is also involved in sending air from the AR to the BC when the BP pressure is decreased, if AR and ER pressures are high. This mode is known as standard braking and is shown in Figures 43 through 45. The system starts out in a fully charged state (charging lap position) with the initial conditions for nodes car and cer set to a high value (see Appendix C for values). Power is shown as the variable type using line width once again. In Figure 43, the pressure in the BP has decreased, which causes the main diaphragm to shif t in the opposite direction from when charging, opening the BC inlet valve. Power can be seen to be flowing into node cbc and also some power is lost to the BP as AR pressure tries to equalize with BP pressure. Figure 44 shows the system when BP pressure has stabilized at a lower value. The AR is still losing energy to the BP. Figure 45 shows flow decreasing to the point where the system will once again be in lap position, but at a lower overall pressure. .... . .sfi.e§¢t: 3%. . . vumUAlmAMvX~MIvvq Luwu Tm... .. ”VA /9. mm Figure 44. Power Response for Air Brake Model Braking Mode (Time = 14.1). lOl .............. ......................... 303v; «oomv~.~ 0068.0 Igfifi .mééwfim..§. .. vumuqlvxfilvv; Lumo 7w... An\m\_ /VL v37 \ ML m. N. NL NxL vau .....wvmm.w Log. L Alt. 79.le HmLom 7,, we: «..qu «n - Namu on NxLfi LLmO mvll «LL m«\\ \.\ m3 ..Qmu / . / .L \ muwnWM.‘ MXH NXuoINIIVNquQ. an LmUOIiVLmH me ilillali \ umO -IIIIVEummm on on“; SA 3 A.» x... ...: \ ., Q: meU Ill MOO 00 I'll wQU LmO ovLmUU /./. 0.3 now La IL ummL ~ 7 cm L / mo \ .. NS / ./ 1L m... i .\ m2 lineiliv _ c on - . Mm. , n. owx/ n~ n / / R umu x... Ilv x; r.// ,;_m. .4.-- m3 4 / ...n S -x/ ..3 gallilvtafli: v.9. /// 3. 8. Eomkmo / A an :7, ---/Ir UuAIIIo x34 8 "Loo; . Lmu nnwo n \ an; mmoo NMVmuo mXL Mmlmed m3 7 ma Ml mx u/MWI QOU .. Ow UDO 4d! UDU me x Emumu Ego laIVonm.) NBC 85 Iowa... 3.... 00/ x Q7 Q- ..R\\n‘ 3 NLw 2 c: ...: 8v . mm. mm: mm. mm... 98 ...... and V a. [no/ no; ”in? \ -.\\x mmumuiflvmmx Aflmmamu 83qu El I.l||vz Rum“. Figure 45. Power Response for Air Brake Model Braking Mode (Time = 19.95). 102 Recharging. After a standard braking application, when the system is in service lap position, an increase in BP pressure should cause release of BC pressure to the atmosphere to end the braking action. Also, the AR should be recharged from the B? to ready the system for the next braking action. The Service Accelerated Release Valve contributes to this recharging initially by sending ER air into the BP for AR recharging. Figures 46 through 49 show accelerated recharge with the flow variable shown as line width variation. In Figure 46, the pressure in the BP (sebp) is starting to increase, which causes flow from cbc to seatm. In this figure the wider line widths around the 1x21 node also indicate that the check valve of the Service Accelerated Release Valve is moving to a new position to allow flow through the valve. Figure 47 shows the system at a later time when the flow out of the BC has increased and a small amount of flow can be seen to occur from ER to BP through the Service Accelerated Release Valve. Figure 48 shows the response as the BP pressure continues to increase. The BC is still emptying while air is starting to flow from the BP to recharge the AR. Finally, Figure 49 shows the response after the BP has steadied out at its maximum pressure level. Small amounts of flow are still occurring. Soon the system returns to lap position. 103 ............. .............. “Hg §§.. 'i‘ 5 a; Is. I". W o O i wov.» $2.: 9 ... :wcox ' q'v'~'u‘v"~‘ ’.'.‘.'-'.‘.' - - ..- S '- miaxz :z-aszzzzEéaezmm vumullvlll va IIIIV v4 9\...... .. .. .. ....wufinwv...~... ..... ..Mw” Hum... . sunny. Han. ...... ...r..u.u.u.u.u... wrummamx ..Ha. Lumu HmLH '37 “\I ML mH NH NL NXL vomu LmXL Alollli Hm Lm Ali 3me 7 /.... a on 9: Memo «n - N mu NXLH LLmo mu? H... L Lomo ManWAN/ X X omit WU A DH/rLWU .IanAm m m l Mina—H NAH 3 Nu R 908 L H/ m H w o no « Summm 8 8 moo m MNI moo no IWIV man Lmo .Lmoo . //x. a. oLH $4.5 “8.. /n Lmo I \.,\2 2: Lou ..N B L V pwo/ xLHMi xL me.mwall mmH QLMMHVXH AiuquluvH VHUL /,i//- no" can VX:A /[ an 3.. /;.r mo mu 4 UUAIIO JUH VHLMOIiVLmU 00A 0' m« \\\V T v on mwuu iv moo n \\I\wfl_ II. myLH 8 an ... ..z mH All. nmXH iv mamo mL nn\ I/mmeu U00 1 UDU iii! HQDO .|.||v QDom a a Iv N QHWIN no 3 HNXL .7 K ...L/ a 8 NLm 2 QQH .... .1. a . mmL wwwu NNH NNxL so HNH Hmmm HNL no/ «a? mug? \un\ Nmumo Alvwli NNx Ilmmiv Nmamu Hmomodwi meH ill! kumu n X 2.85). Figure 46. How Response for Air Brake Model Recharging Mode (Time 104 Illllllll . -~v-'-:-;_-:-.::-:-:::~:~rats-qr. ML 2 NH .3... . ._ mmou 9&3 800 MN! m n... Joli 93 iv mama ago a\ :98 / H, ...I Q \nv H v3 / m3\ .- I NL NXL v mu Lm m VL LmXLmfialIl HmL IIII. HmLmu vn a: U o. «a can \ w / v39 02/; mama 3 NXLH LLmo IIV vxL Lamu L / A N? Nu \ 8 3 an NxH IMHIVNumuR LOUOoflvLmH mmH no .535 «Y / iumlr muo LLmo Lmuu 3 /. ”.9: EH 19mm... / LWO I ...wU umu / xLH ml xL a . .51....” 23 L dill“ xH All a» All. LWH 0» "UL /;///. no. 93 \«D; f /' 98 mo 2 H i Zoo .3 2 ' mmou molv moo .- 0.2 M! meH n... / 8 231 08 Hugo IIIv doom A: mL . NanHmI «ago 35 I185 .7 H3\ .7... \ 8 NLm as 2H s: s. NNL mm: mm. ~wa 93 Siam... \HNL HMO/«o? \ ”a HMM\\ mmamuaflimmx INIVNNQmu Hmamudkaidlulllmumu Figure 47. Flow Response for Air Brake Model Recharging Mode (Time = 5.4). 105 ' o N ”mink . N k ”Otwodom norg.« nor”0.« Herman. u o d ltH a: § 3-80.0 xiuou.~ 8.80.0 4’.- 6%. ...? uwsfimfiavfi 3.... .. . 3&3... ....... ..L. a ......r ..................... { ......rk.......\.. vvaAlnii fix“ inf VH ...qu .TwLH ML 2 NH NL NxL vowu SAWM“. meLmIiII HmeaflH 3me 37 .29 nfi/r Memo 3 - mamo meH LLmomlvvaL 2 Lomu . .7 .\ ../ ... m m fimxH NxHIImMIIINumu an LmuomnIVLmH moo om.— m~.._ no m. 3/ u u in L m MIN 0 0 ..~ A..Vo//Lm.oo1//...w./ 2 L panicN xLH Mic... L Xaqikwflioilhun on umu m3.» mowau/ H A A meU illnmUO n 3v mamo mH AllmxH iv vu/mr. anMn\ 3...”..me Q a IIIV . N andiIN no] / VHNLO an HNXL om on NLQR: on QDHR n: 8? L/NNL... mm. ~me 9.6 8.5mm \ EL 8—. {A a \\ mMumuimeHBIMwiv NNamu Hmawu L Hm; Awmfli Hmtmu Figure 48. Flow Response for Air Brake Model Recharging Mode (Time = 9.45). 106 vumuiflivxaiva Lumu amLa «3%... ..7 mL .2 N. mg mi 38 m E .6? infill E: Mull ELQm 6/ van», .«/r Mumu/ «N Namu on in LLmo i «...L 2 no Lamu NV \ A wn/r «L mamumiv mxH Nxa AllolalliiNvmu R LmuomoNVLg/ mmfiiiNFi oumolsumam 8? 8? #v0/ lerO 93 V Lmu ....N R u xL mm. umu / “Mmil XL meLooAmli \W S u u o L an Ex“ up no 4‘: mm nmaL /3 , nmo mo 3 . UUAIIIO v.3 i «LmOIlllllemu 000...: l me: P m... Be n 9 \\V 8v v . .umauMimuo - \\my\.L4ilmx.; I hoN 3? 1h ........................... k ma Mimi/mm muwu uno ”50‘.qu onu EU..~ m no.5.“ III. I . man: Nano suo 3.5 i 8.... 3&9 « NI 4 on Ii I . l/ x / «..\ 88; km a on 8 Nkm an an Qflamr new 3&8; out i I .. 3&3; NNL Nng N” NNXL QEU “NH “mum. \ «mL . [1.0/1 «0; KW. ”Irv .\\ III 3.8. n N93 mwi mmx 4ii| Nmamu 5%... lim 8. H H........lii 8me 3185;. E z I 00.80... >8. Figure 49. Flow Response for Air Brake Model Recharging Mode (Time = 14.4). 107 Manual release. From any lap position the option should always be available to manually release the pressure from the AR and the ER. When AR pressure decreases this will also cause release of the BC, assuming that BP pressure remains fixed. Figure 50 shows this occurrence. The power variable is displayed with line width variation. The force input serel is increased by a set amount to cause the manual release valve to move up from its valve seat, creating a flow path from ER and AR to atmosphere. It can be seen on the graph that power is high along the paths from car and cer to seatm. Nearly all of this power is dissipated in the flow resistances (rxar and rxer). The power is low on the bonds connected to Oat because the atmospheric pressure is a very small value compared to AR and ER pressures. A small flow also occurs along the path from cbc to seatm. In Figure 51, AR and ER pressures have decreased to the point that flow into the system from 8? starts to occur. If the system were held in this position with the manual release valve held open, pressures would all stabilize to that of the BP, and a constant flow would occur from 8? out to atmosphere. 108 comm . N . .. . 5.35. .... u me: D” "O.N k3 Iva o.~ «a; ..— .« l5? 0+ I meow—”o. .— Noowong 3&3.» ~0o3n.~ 8930.0 rug .gf'FmT-f-I- Edit-$7495???X‘E'C‘HJFNEWW . . . ..I‘II-Jll_._.'...'.'._ 444:3:3:T:?:-‘.‘?i$.fi':‘-:3:7:?:5: '.‘.\'.'-'.'.'-'.‘ u - r u u l I ‘.‘~:.'.-.'.-.'.‘ NXL Vumulwvlvvxfi in: Lumo 3.: anu T n. N. N. v m .53. ..L .x. x a on '39 v3 mVA Mamubwnlmzmxu nwammumo o.» Lmoo umo lnlllv Eummw L an 3 8 8 o. 8 ‘mefl ‘ mmau IIL~|ll moo uo l.iz..ilv mau wa/ Lmou LmH / o: 2: mm.— mL awed! ummL / A :n 7 5. I? L80 .5... mu 3 a 77/- H Xr—OM 1.... mod / an Lflixfidllowiuuflllu: 03 o Qm%3Wo S/r L no II! 0 m3 «LNOII LMU v 3 w v mmuowulnmuo n xLaAml mnxLfi 3 ... / m.H I'm: imamu ago . 3 uncalllunu «0 mo [Mm mL>\ a mumo mg: m. anneal «LE: 4 neuohl n2 i 3.5 i 8.: 8 Ah on V 8‘8 Ataé NNL mm: mm. 8.: s a. 3mm Na. /.. yOé \ QEU fink/Huh? WA\\ A Q JQ , x 8.8... mmlsiimm 8 r. Bi... 8 H .. 3&8 Figure 50. Power Response for Air Brake Model Release Mode (Time = 2.25). 109 ..... ....x. 9.9. Mug. 9... .... «29w. .wflwx ..9.. ..L. “was. 3%.. .wewémw 99.3.“)? ..L.. 9... «9999L9 .............. ....v ..... ...-“AC... 99 wow MWNlflllV: HMO lily Eummm Mod L iVum L mL 3 m. LQt me vumodivxLflvL Luwu ELL Lqmu \ L. 9 mL 2 NL NL on Emu. Lwwa. LLL V: v3 ./ mumu7Hn/wn - Nomu NxLL LLmomuvvxL LmXLAlllquLlliLmme ‘ 4/ mama Amel meNxL Ham Numu Lmuo L Ln fig ON :/ LMXfl OWN\\ «CuA mmauAMllmoo ool.~lvmau Lmo Lmou L2 8. 8 mg L L L .../L b LmC‘ L uwu/ 2.. L3 L L/delluunlLLuL a VUL L L. o amooxmmo “L/ L r mmuo Luinmuo 3.. mm; Al me lir muwu 9... [mm mLLN 3 mpmo ano ... mu u Alllud no 3 L ill Lunol BL... « ELL 4 «cool NLmLs 4 asuo. .Ll 9L: i 8.6 i LNXL < NNL my“ m9 no «we NNXL NNumUv A. NNxL li NNQwU 8‘ LL ....e t— rd mem 8.. QEU ,,/ Lmamui LNLL i Lmumu on tn Figure 51. Power Response for Air Brake Model Release Mode (Time = 4.2). 110 » ..4' Mia] it} iidd'll: l' unsgflufi MNIHWJ. wlifl . .'-)p¢ 54H v‘h; 9:3’:?i‘m.’.; 333 u " «s “1* 33";4 mo» 'i’r‘f; "H ‘. ':= . - n ' 1? . “>‘.}"2;v' . ‘i ‘7' 9‘ n2.“ .." 3 .:'=.._ “592'” .711. .'=: M l 3 ms7a‘r-wngkr‘u[i'figmigmigé rum-rntfwri:f‘lfficw'vtutfium;{Hr-.ti‘imnrnEL; k1/2 k1/2 I 1.: ..JH. n. _ ‘ ' T l. 1‘ it ?. =-::;i " 'I:I;.,- .5"! 1 ' .. n u.) ;: '3 I" “ " ‘ “' '. "l '9 P". ‘1 ‘3‘” d. . :1 “l.“ .: .t 9‘ ._l’, it .9 . .L; . 'l.‘ ...‘1 ll: ‘ ' i" " '3 . i ‘ ' “ " ‘ ' .i $5.. ._ .. My. . . ‘ . '. “.7 -. . .... w ‘ l-E‘i zll‘li'2l3.,' ”JILL. =: .1"'..E '.. ’.—'.' -».:‘ ‘.‘ ‘J.:.‘ .» " . ' -."Vl* . w . H: w . pun '_, . xv .. -' ~|..’ . ,, x3 k2/2 k2/2 W iii. ' l L l ’ :- 44 t1 u I k3/2 k3/2 Y( ) Base Figure 52. Schematic of Mechanical Three DOF System. 5.3 Modal Analysis Example In addition to applying visualization techniques to industrial scale systems design problems, there is also usefulness in extending the concepts to educational problems, in order to aid students in their understanding of basic phenomena. One of these educational applications of visualization is modal analysis in vibrating systems. Mathematical models of systems with several degrees of freedom can be used to determine system natural frequencies and mode shapes. The mode shape is a description of how a system vibrates when it is operated at or near one of its natural frequencies. The BGVis-ZD tool can be useful in helping students to "picture" the different mode shapes of a system and understand the actual time response better. An example three degree of freedom (DOF) mechanical system used to illustrate how the dynamic display can show mode shapes is shown in Figure 52. In this system three masses are connected together with linear springs. Each mass is allowed to translate in the x direction. The system is connected to a base, which can be used as a 111 source of motion for the system, but for this example which will involve natural vibrations, the base is fixed in place. A bond graph of this system is shown in Figure 53. Each 1 element along with the corresponding I element represents the velocity of a mass. The C elements model the springs between each mass. All of the elements are linear, with the masses of the bodies 1, 2, and 3 equal to 1 kg, 2 kg, and 2 kg, respectively. The C element stiffnesses are 1 Wm for C1, 1 N/m for C2, and 2 Wm for C3. The bond graph is set up to conform to the geometry of the actual system, to aid in the visualization. The model file including the equations for this example can be found in Appendix C. 1x1-—A 11 CIT—01 1x2—> 12 C2'<——— 02 1X3—-—\13 C3<——O3 1Y<—-—SF Figure 53. Bond Graph of Mechanical Three DOF System. ENPORT was used to determine the three unique eigenvalues (natural frequencies) and eigenvectors (mode shapes) of the mechanical three DOF system. The eigenvalue and eigenvector values calculated are shown in Table 4. When an eigenvector is used as the initial condition for a simulation of the natural response, the system experiences the natural mode of vibration corresponding to that eigenvector. Simulations of the time response for the three different modes of this system were completed and the results were visualized using the BGVis-2D display environment. l 12 Table 4. Eigenvalues/vectors of Mechanical Three DOF System. genvector Figure 54 shows the response of the flow variable type displayed at a time when the flows are near their maximum. Since the response is sinusoidal, the displacements of the masses are also sinusoidal functions with the same frequency and amplitudes all scaled by the natural frequency. The line widths on bonds 1, 2, and 3 illustrate the first mode shape for the system. During the course of the time response the overall values rise and fall, but the relationship between the displacements of masses 1, 2, and 3 stays the same. Mass 1 experiences the greatest displacement, with mass 2 experiencing a somewhat less displacement in the same direction, and mass 3 has the least displacement also in the same direction. Watching the levels of the glyph symbols allows the student to track how energy is shifted between kinetic energy (I elements) and stored energy in the springs (C elements) during the course of the animation. Figure 55 shows the second mode shape. In this mode masses 2 and 3 move together, but with the displacement of mass 2 at about half the value of mass 3, while mass 1 moves in the opposite direction with a displacement value near that of mass 3. Figure 56 shows the third mode shape. In this mode masses 1 and 3 experience equal displacements in the same direction, while the displacement of mass 2 is equal and opposite. The advantage of using the dynamic display would be even greater for systems with more degrees of freedom and for systems involving energy domains other than mechanical translation where mode shapes are not as easily visualizable (e. g. electrical). 113 ”a””um””n“mummy“Layman”... ”an””Wynn””up.”unfinuwwfiwwaw».9”.9u”myL”my....”wfin”.....munmwwwwwwmnnuwwwuuuwmqmManama nwflwwwwfl.th.L.n..wywfiuwnumflwwwmnwunwni. ...wu......mwumwwwflfiuwmmmmmwwmuwwunwxw. ......«xfixgfig9fixr3awxy ..L..9.....L. .3, ...............v.....r.....q........9mr......\.A.....ufi.............rb......................... .4.....,.........................q...9L...............v..............9.......Lu.r....u..u...4.94.999...“ .................. é. ............. .............. lllgl is. §. is H at ? § 3? 95.5. 5| § 3.806 L Figure 54. Flow Variable Display Showing First Mode Shape. 114 ...?”yawnxaakuvfinvq.}m. 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Chapter 6 Visualization Example Using BGVis-BD The three degree-of-freedom BPR car and suspensions bond graph model representation was extended to three dimensions using the three-dimensional bond graph display environment (BGVis-3D). The 3-D bond graph representation of the BPR model is shown in Figure 57. The 3-D representation can be seen to have the same connectivity as the 2-D version, but clearly the 3-D representation corresponds more closely to the geometry of the schematic (refer to Figure 12). The suspension branches and the rotation/translation axes are much easier to associate with their corresponding locations in the schematic, so much so that it may no longer be necessary to keep the schematic nearby for constant reference. Figures 58 through 61 show the same power response obtained from the model of chapter 5 with a pothole input visualized in the 3-D environment. Color variation is used to show the power values on the bonds. Figure 58 shows the expansion stage of the right/front branch at the beginning of the pothole. Figure 59 shows a later time stage when energy is being damped out of the front branch after the front tire has passed the pothole. Figure 60 shows the effect of the rear tire encountering the pothole and Figure 61 shows the damping out of this energy in branch 3. Combining the response data with a 3—D representation of the bond graph model lessens the amount of work required by the modeler to visualize the response with respect to the schematic and therefore the physical system itself. 116 117 Figure 57. 3-D Bond Graph Representation of Car and Suspensrons Model. 118 Figure 58. 3-D Dynamic Display of Response to Pothole Input (Time = 0.112). ll9 Figure 59. 3-D Dynamic Display of Response to Pothole Input (Time = 0.115). n. ..oi'df.‘ on". I‘ll... - 1.11:1... . . ._ . PM 120 Figure 60. 3-D Dynamic Display of Response to Pothole Input (Time = 0.300). 121 Figure 61. 3-D Dynamic Display of Response to Pothole Input (Time = 0.305). Chapter 7 Conclusions 7.1 Summary of Contributions The research work completed has made a significant contribution to the use of bond graphs in modeling and design of large-scale systems. The principal research objective of designing and implementing an improved design environment for engineering systems based on the use of bond graph methods as a structured modeling technique, which makes the interpretation of dynamic system response easier for designers, has been achieved. 7.1. 1 Two-Dimensional Visualization The BGVis-2D environment provides the dynamic link between model response data and bond graph structure which is necessary to take advantage of the knowledge of the system that the bond graph supplies to the engineer. This link between simulation data and bond graph model makes the visualization of response more meaningful. This is especially useful in the process of gaining insight about model behavior. The environment is also very valuable in assisting in the task of explaining complicated system behavior to those who are not familiar with an existing system model. The visualization provides a way to communicate how the system is behaving in a basically qualitative way. 122 123 The primary functions implemented in the BGVis-2D display environment were: 1) loading of bond graph model files into the data post-processor; 2) integration of effort and flow variables with respect to time to obtain the net energy variables explicitly; 3) three different scaling options for data; 4) bond color and width variation for a display of bond graph variables including power as if they were flowing on the graph; 5) glyph display for a level-type display of associated energy values in the energy storing and dissipating elements of the bond graph; 6) time controls necessary to control the display of the animation at the user's discretion. Two practical engineering system examples, an automobile in bounce-pitch-roll mode and a railcar airbrake switching system, were developed to illustrate the use of the BGVis-2D tool. 7.1.2 Three-Dimensional Visualization The BGVis-3D environment provides a stronger link between the bond graph and the physical system by allowing display of three-dimensional representations of bond graphs. Matching key points in the bond graph and physical schematic further enhances the link between the physical system and the model behavior. The computer graphics standard PHIGS was used to implement the functions of the graphical display. A method for translating bond graphs into three-dimensional objects using spheres for nodes and cylinders with arrows for bonds was established. The primary functions implemented in the BGVis-3D display environment, in addition to some of those mentioned above in the 2-D environment description, were: 1) loading of 3-D bond graph model files and data files into the environment; 2) control of the viewing parameters, including changing the angle of view and the distance from which the 3-D bond graph is viewed 3) color variation to show values of bond graph 124 variables including power and energy on the graph. The automobile example was extended to three dimensions to show the capabilities of the BGVis-3D environment. 7 .2 Areas for Further Research Several areas have been identified as possibilities for future research. An overall goal of future research might be working toward what has been called ”interactive quantitative visualization” or "computational steering" (Peskin, et al, 1991). The basic idea behind these concepts is to graphically link the model with results during computation so the designer can make decisions about the quality of the model as the computation progresses. The suggested future research areas are grouped into two categories, the first relating primarily to the BGVis-ZD environment, the second to the BGVis-3D environment. Regarding the two-dimensional bond graph visualization, the following areas warrant further attention. 1. The integration of macro-modeling capabilities and library storage of sub- components with the new display capabilities would be welcome. In this way large systems could be expressed in bond graph form without having to see all the individual details of each subcomponent. Elements in close geometric proximity could be grouped to make the power animation clearer. 2. Additional scaling options for variables could be implemented to show behavior in the clearest way possible. Scaling of variables by energy domain might be helpful to distinguish between variable levels which vary greatly over the different energy domains. Power and energy can be directly equated across the domains if 125 appropriate units are used, but individual variables have their own units in each domain. For example, considering the behavior of the airbrake switching system, the efforts in the hydraulic sections are numerically large, while the forces on the mechanical parts are very small in comparison. If all the efforts are scaled together, the relative values of forces on different mechanical components is obscured. If the mechanical efforts could be scaled independently of the hydraulic efforts, better relative comparisons could be made. 3. The capability for including multibonds in the graph should be added to the ENPORT modeling software. A multibond is a concise way to represent a natural grouping of single bonds (Breedveld, 1985). Although multibonds do not necessarily aid in helping bond graphs to correspond to natural geometry at a detailed level, they can sometimes be of great help in simplifying graphs at the macro level. 4. It would be desirable to show in the animation not only information related to each specific instant in time, but to include some time history information as well. In this way still prints or photographs of different time stages would show power data related to several previous and following time stages, allowing for better interpretation of dynamic response without having to view an entire animation sequence. 5. It would be useful to transfer the functions of the 2-D environment described in this thesis from the UNIX version of ENPORT to the more widely disseminated PC- DOS version. More powerful PC's such as Pentium and Power-PC based machines make the animation realizable in the PC environment and would therefore make it available to many more engineers to aid in their system design work. 126 6. The files used to store the simulation results data are often very large due to the fact that all efforts and flows for all bonds over all time stages is stored along with the state variables. A certain amount of this information is redundant due to bond graph constraints. For example, all of the efforts on bonds connected to the same zero-junction are constrained to be equal. It might be useful to establish a format for output data files which compresses the files by eliminating all redundant information. Reconstruction of the data could be performed in the visualization postprocessor. In addition to the 2-D list, the following suggestions for future research apply for the three-dimensional bond graph visualization. 1. Since the goal of this research was to show the effectiveness of display of simulated behavior data on a 3-D bond graph representation, the activity of 3-D bond graph construction was ignored. In the future it would be useful to develop a 3-D model builder along the lines of the current 2-D model builder 2. To further enhance the correspondence of 3-D bond graph representations to physical systems or schematics it would be useful to develop the concept of anchor points in the bond graph. These points would be specifically intended to refer directly to specified locations in the system. The ability to place and manipulate these anchor point elements would allow the engineer to scale the model with the physical system, as in a CAD drawing environment. 3. In the interest of providing as much information to a designer as possible in a given display, it would be useful to develop an animation of the physical motions of the mechanically translating bodies in the system using bond graph element anchor points in the bond graph display environment. Multibody dynamic mechanical system modelers 127 like ADAMS already use this technique with rigid body models to enhance interpretation of simulation results, and adding this type of display to bond graph models would also be useful. APPENDICES Appendix A A Brief Introduction to Bond Graph Modeling A.1 Bond Graph Variables and Node Types In Chapter 2 of this report, the purpose of bond graph modeling was stated and a general description of bond/system graphs was given. The purpose of this appendix is to provide a few more details about system graphs and the way they are constructed. A bond graph is a graphical representation of the physical behavior of a system leading to an explicit mathematical model involving system variables. A bond represents a power transfer connection which appears at a port, or place where energy is transferred to or from a device. The structure of a bond graph takes advantage of the fact that physical variables in many engineering domains appear as related pairs whose product is power. These power variables are denoted as effort and flow. Related to the power variables, two other types of variables are identified which are of use in determining energies. These are called momentum and displacement. Depending upon which energy domain the power transfer occurs in, the generic variables effort, flow, momentum, and displacement can be assigned to different physical quantities. Table A-1 lists the variable names and units for several common engineering energy domains. A given system can be separated into subcomponents connected at their ports to other subcomponents via bonds. This decomposition can be done at various levels, until at the most precise level, physical behaviors of a subcomponent can be described with a relatively small set of bond graph elements (node types) and their associated constitutive 128 129 equations. The set of standard bond graph modeling elements was shown in Table 2 of Chapter 2 and is repeated here as Table A-2. These elements can be used to describe behaviors found in most engineering system domains. Bond graphs can also be augmented by the addition of block diagram elements and signals. In this way information flow as well as energy flow can be accounted for and control systems can be modeled along with the actual system under study. Signals are different from bonds, since signals by definition carry no power, only information. Signals are represented graphically by using a double arrow rather than the single arrow used on a bond. Some examples of block diagram elements are shown in Figure A-3. Table A-1. Variables in Various Energy Domains. Variable General Mechanical Mechanical Electrical Hydraulic Translation Rotation Effort e(t) F, force T. torque e, voltage P, pressure (Newton) (Newton*meter) flolt) (Pascal) Flow f(t) V, velocity w. angular V61. i, current Q, volume flow rate (meter/second) (radian/second) (Amiere) (meter3/seeond) Momen- P 'f e d P, momentum H. angular mom. 2. flux link. Pp. integral of press. tum (Newton*second) (Newton*m*sec) QVcber) (Pascal *second) Displaee- ‘1 'If m X, distance 9. angle q, charge V, volume merit (meter) (radian) (Coulomb) (meter 3) Power P(t)=e(t)f(t) 130V (t) (W arr) t(t)w(l) (W at!) e(t)i(t) (W att P(t)Q(t) (Watt) Energy E(p)= ff dp fV dP . kinetic [(1) dB , kinetic f. c9. , I Q de . kinetic (Joule) (Joule) (Joule) magnetic (J) (Joule) E(q)= f c dq f F d.\' , potential frde , potential fe dq . f P dV' , potential (Joule) (Joule) (Joule) electric (J) (Joule) Table A-2. Standard Bond Graph Elements. 130 Element Element Bond Graph Constitutive equations Type Name Symbol General Form Linear Form E Sources Source of SE —A E = f (time) E = Constant Effort F Source of SF _E_> F = 1' (time) F = Constant Flow F Passive - 4_E_ - _ a: One-P Resrstance R F E - f (F) E - R F . E E=f(Q) E=l/C*Q Capacrtance C ‘—F— p = dQ/dt F = dQ/dt . E V=f(P) V=1/L*P Inertia I 4?— E = dP/dt E = dP/dt Two-port L _.3 El = n * 132 transducers Transformer Ft TI: F2 F1 = l/n * F2 El [‘2 El = r * F2 __\ Gyrator Fl GY —F2—3 F1 ___ l/r * £2 £1 £3 _ _ Junction One-Junction -—\ l——\ H - F1 - F3 elements Fl F3 EI-EZ-EB = O [-2 Ln El E3 Zero-Junction ‘ 0 \ 131 = 132 = B F' 3 LP, *3 Fl-F2-F3 = o Table A-3. Block Diagram Elements. Element Name Symbol Constitutive equation Signal Source W Y = f (time) Signal Sink No output equation Gain v = K * u Integrator U Y Y = Udt Function U . Y = NU) Transfer Function U Y Y = T(s) * U Summer Distri butor Y=U1+U2+U3 Y1: U. Y2 = U. Y3 = L' 131 A.2 Standard Procedures for Modeling Because bond graphs have been developed with the goal of allowing structured heirarchical decomposition of a system, straightforward methods can be used to translate schematic diagrams into bond graph models. The methods differ depending on the energy domain being modeled, and several of these methods for handling common domains will be detailed in the following sections, along with simple examples. The general steps for obtaining a bond graph from a schematic are: 1) establish a coordinate system and unique system variables for the system to be modeled; 2) follow the appropriate procedure to obtain bond graph model with appropriate signs on bonds; and 3) define causality to establish input/output relationships within model in order to prepare for algorithmic equation derivation. This section outlines the establishment of coordinate systems and modeling procedures for mechanical, electrical, and hydraulic systems. Causality considerations will be discussed in a later section. Mechanical Translation and Rotation. The procedure for obtaining a bond graph model of a mechanical translational system consists of the following steps. First, identify all unique velocities in the system (flows) and choose the positive directions for each velocity and its associated force (effort). The positive power direction occurs when both of the previous quantities are positive. Next, establish a l-junction for each unique velocity. Attach necessary inertia elements to their appropriate l-junctions, along with sources of force or velocity. Finally, connect in compliance and damping effects with O- junctions in between the appropriate l-junctions. Figure A-l shows a simple mechanical system schematic and its bond graph representation. The l-junction indicates that a common velocity (V) exists for several different effects, and that the forces generated by these effects on the mass must add up to 132 zero. The effects suggested by the schematic are the input force on the body (Se), the compliance effect of the spring (C), the resistance effect of the damper (R), and the force due to the inertia of the body (I). Mechanical rotational systems follow the same procedure, but linear velocities are replaced by angular velocities (flows) and forces are replaced by torques (efforts). x (V,a) F(t) Se IV C/ 1V \ I R Figure A-I. Mechanical Translation Example. Electrical Networks. There are two different ways to approach electrical model building. The first is to use I-junctions (common current) for electrical elements in series and O-junctions (common voltage) for electrical elements in parallel, and construct the entire model by observation. Another procedure, called the circuit-construction method. is more straightforward. The procedure starts with establishing positive directions for currents in the circuit. Next, all unique voltages are identified, and a O-junction is established for each unique voltage. All other circuit elements are connected into this structure with l-junctions between appropriate voltages. It is finally necessary to choose 133 one voltage as ground, eliminate that O-junction, and simplify the graph as much as possible. A simple circuit example is shown in Figure A-2. The l-junction represents the common current (i) in the circuit, with all the voltage drops around the loop adding to zero. The effects indicated in the schematic are the voltage source (Se), the electrical resistor (R), the electrical capacitor (C), and the electrical inductance (I). Se \ / , Figure A-2. Electrical Example. Hydraulic Circuits. Bond graph models can also be used to represent hydraulic/pneumatic circuits. The procedure used is similar to that for electrical circuits, but currents are replaced by volume flow rates (flows) and voltages are replaced by 134 pressures (efforts). First, the positive directions for volume flow rates (Q's) should be established. Next, O-junctions should be used to represent each unique pressure in the system. Storage (C) elements can be placed on their appropriate O-junctions, and all other hydraulic elements can be added in with l-junctions connected between the appropriate 0- junctions. Figure A-3 shows a hydraulic pump system example. The pump itself transforms mechanical power (t, w) to hydraulic power (P, Q). There are two unique pressures in the system: the inlet pressure (03), and the outlet pressure (Ob). The l-junction determines the difference between the two pressures and relates that value to the mechanical input through the transformer (TF). Pb, Q Pa, Q Ob Pb _t__x TF__s. 1 Q ‘9 (lzT) Pa 0a Figure A-3. Hydraulic Circuit Example. I35 A.3 Causality Assignment Once a system bond graph has been constructed, it is necessary to establish a system of input and output relationships in order to make the composition of the constitutive equations of the elements into a set of system differential equations more direct. Applying causality provides a structured way to develop system differential equations. A causal stroke on each bond is used to indicate in which direction the flow is the input, and therefore in which direction the effort is an output. With the causal stroke placed on the left for the following elements A l \ B it can be inferred that the flow variable is the input to element B, and conversely, the effort is the output from element B. From the point of view of element A, effort is the input, and flow is the output. Different element types have different restrictions placed upon where the causal strokes can be placed. Table A-4 lists the available causalities for each element type. Table A-4. Causality Possibilites for Bond Graph Elements. Source Elements SC—‘l SIP—- Passive Elements I ——"I Integral causality c I——— Integral causality R l-—— R ——I Two-port Elements —-l TF —'1 F'— TFl'-—— ——4 GY l— l—- GY ———-| Junction Elements T i ——-lo——-I t 1} 136 A.4 Multi-Domain Example In order to show the methodology of bond graph modeling for multi-domain systems, an example is presented here. Each part of the system in a given domain is modeled using the previously mentioned methods. The connections between domains are provided by transformers or modulated source elements. The example system is the Radar Pedestal Position Control System shown in Figure A-4. The system consists of a radar pedestal which supports a radar dish which is allowed to rotate about the z-axis. In order for the radar to track objects accurately, it is necessary to carefully control the position of the pedestal by means of a motor supplying a torque and angular velocity through a shaft and gearing system. A partial decomposition of the system into subcomponents is shown in Figure A-S. A complete system graph is shown in Figure A-6. In the complete system graph element names ending in E are part of the electrical circuit driving the motor. Specifically, IE and RE are the inductance and resistance of the motor circuit respectively. Element names ending in M are part of the mechanical part of the system, including a shaft with compliance and gearing system for speed reduction. Specifically, 1M and RM are the inertia and damping in the motor, CS is the shaft compliance, TF represents the speed reducing gears, IP is the load inertia, and RP is the bearing friction of the load. The block diagram elements provide the control action to be applied to the circuit controlling the motor speed. The variable w is the angular speed of the pedestal, and theta is the position of the pedestal, calculated by integrating the speed signal. Causality is also shown on the diagram. The system's equations have been derived using the computer program ENPORT, and the response of this system to a step increase is shown in Figure A-7. Command Signal (reference value) Figure A-4. Schematic of the Radar Pedestal Control System. Control Action Electrical Motor Motor and Gear Speed Pedestal C i— —- ~- Figure A-S. Section (macro) bond graph as illustration of hierarchical decomposition. 138 llllllll ...?! such-.58... IVIIUOI l 'I” Figure A-6. Bond Graph of the Radar Pedestal System. 6.40 3.20 4.80 TUESZALE I. LEE“)! “EM —'2 ""‘E.S3 xtlE Figure A-7. Response to a Step Input. Appendix B Program Code 8.] Two-Dimensional Environment The software developed for this application is stored in a file called dyndis.c. It is necessary to compile this along with the ENPORT library routines stored in Iibenp.a and the file mainpp.c which contains the main program. 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UIAAuN .N A INdU . 0000000000 000 00AAIC .C A 0040 Ah. 00AA:C .0 A 0040 . 0000000000 ONN 00AA-N .N A INAG Ah. UCAAJN .N A [Ada . 0000000000 CCN 00AA;N .N A [Add FC- 00AACN .N A IAAG . 000 0000000 Cam. «0.00.0. 0A 0:0 0:0 Cu. 00AAI» .00A0030. N. .006. huN 00AAI» .00A00§ IA .000. on. 00AAIN .00A00a. NA .000. AoN 00AAIN .00A 003. 0A .000. CCN 00AAUN .00A0000. AC. 00AAIN . 00A 00... hANh .000. ACN 00AA1N .00A00000 AC. 00AAub .00A000O. AANN .000. AhN 00AAir . 00A 000.. or. 00AAIN .00A00‘. NAACP .000. CDN 00AAIN . 00A 00‘. co. 00AA1N . 00A 00.6. NAANN .000. hCN 00AA h .00A0000. CC. 00AA-N .0030... NBA: .000. 000.0m03000 REFERENCES REFERENCES ADAMS - Automatic Dynamic Analysis of Mechanical Systems - User's Manual. Ann Arbor, Mi: Mechanical Dynamics, Inc., 1989. ANSYS - Engineering Analysis System - User's Manual. Houston, PA: Swanson Analysis Systems, Inc., 1993. Arora, J. 8. Introduction to Optimum Design. MacGraw-Hill, Inc.: New York, 1989, ch. 1. Arnold, D. B., and D. A. Duce. 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