DOCTORAL DISSERTATION SERIES titlesmttesis of a z m U n a M M w o n m -c m ii' P tM e . m m t n m m m a p m m tb m c rm of F & m m p pm a u th o r MMH HikotkTtifcAMtk UNIVERSITY M/C//' DEGREE m STM COiL DATE PUBLICATION NO. i y UNIVERSITY MICROFILMS A kl kl A D D A D /^ 5 / SYNTHESIS OP A RESISTANCE - CAPACITANCE FILTER WHOSE POWER INSERTION RATIO APPROXIMATES A PRESCRIBED FUNCTION OF FREQUENCY BY NOAH HERBERT KRAMER A THESIS ubmitted to the School of* Graduate Studies of Michigan State College of Agriculture and Applied Science in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Electrical Engineering 1951 To Dr. J. A. Strelzoff, whose help and encouragement made this thesis possible INTRODUCTION (1) NETWORK SYNTHESIS. There are several aspects to the gen­ eral field of Network Syn t h e s i s . One interesting facet is the Approxi­ mation problem. The desired characteristic is usually given in a graphical form. The problem requires the construction of a mathematical e x ­ pression to describe a network that possesses the desired characteristic, within a permissible approximation. Elliptic functions, Tschebychef polynomials, and Butterworth functions often appear in this type problem. Another aspect of synthesis is the Real­ ization Problem. What mathematical or graphical functions can lead to a physically realizable ne t ­ work? What geometric forms can this network assume? Much of the pioneer work in the Realization Problem has been done by 0. Brune. (1) This thesis will deal with both aspects of Network Synthesis. 1 Brune, 0. Synthesis of a Finite Two Terminal Network Whose Driving Point Impedance is a prescribed function of Frequency. Journal of Math and P h y s ., vol. 10, ppll91-235 In this thesis, the response or an ideal filter Is approximated by a mathematical expres­ sion (Approximation problem). This expression is used to realize a symmetrical lattice, composed of resistances and capacitances (Realization p r o b l e m ) . The restriction to these two elements is not Just an academic choice. R - C (Resistance- Capacltance) networks can be designed to give many responses, and the additional loss that they intro­ duce, due to dissipation in the resistances, compensated by subsequent amplification. can be In many cases, where only a frequency discriminating cir­ cuit Is desired, the loss introduced by the resis­ tances is of no importance and can be ignored. The exclusion of inductances might introduce economic and construction advantages. Certainly the problem of magnetic pickup is reduced when there are no In­ ductances . The terminology in Network Synthesis has become confused, since Mathematicians, physicists, and Engineers are all contributing to the field. Is advisable to clarify terms at this point. -2- It (2) POUR TERMINAL NETWORKS A Pour Terminal Network, or Quadripole, has a pair or terminals designated as Input, and the other pair designated as Output. Associated with the input terminals are the Input Voltage E^and the Input Current 1^. The output terminals provide Output voltage and Output Current I . In the usual case a generator E with an in­ ternal Generator Impedance Z^ is connected to the input. A Load Impedance Z2 is connected to the output. This thesis restricts these impedances to pure resistances R and R . 1 2 Figure 1 Illustrates the notation that will be employed. Since the direction of the currents is arbitrary, the notation shown is chosen. I Z I FOUR TERMINAL E E E Figure 1 NETWORK Four Terminal Network with Load. _ - 3 - Z (3) NETWORK RELATIONS The relations between the input current and voltage, and the output current and voltage are found In any reference on Network Theory - 2,3*4. I1 - y ll E l * y l2E2 E 1 - zllIi + Z12I2 Eq.1 X2 -= y 21 E 1 4-y22E 2 E q .2 E2 - z 21Z1 + Z2 2 I2 y l l ,y22 are the short circuit driving point admittances. y12*y21 are the short circuit transfer admittances. zl l ,z22 are tlrie °Pen circuit driving point impedances. z12*z21 are °Pen circuit transfer impedances. In a passive network y ^2 - y21* z12 “ Z2 1 * Gewertz (5) has shown how the four admittances or impedances uniquely characterize a network, and has set up realization techniques when these para­ meters are known. 2 Guillemln, Ernst A. Communication Networks Vol. II 1935 New York: John Wiley 3 Guillemin, Ernst A. Communication Networks Vol. II 1935 New York: John Wiley 4 Everitt, W. L. Communication Engineering Second Edition 1937 New York McGraw-Hill 5 Gewertz Synthesis of a Finite Four Terminal Network Jour. Math and P h y s . Vol. 12 1932 - 1933 PP. 1-257 -4- (4) TRANSFER IMPEDANCE Consider the generator impedance and the load impedance absorbed in the quadripole, as in figure 2 The ratio of the generator voltage to the load cur­ rent is E/l. This ratio is defined to be the Trans­ fer Impedance of the quadripole. New Four Terminal Network Figure 2 T E, f Quadripole for Transfer Impedance The output voltage of E^ of this quadripole Is zero, for there Is a short circuit across the new output terminals. Also E * E1 . When these values are inserted into equation 2, there Is obtained X2 = E ly 21 Zt * e/ I2 “ 1/ y 21 Assuming a passive circuit. 1/ y!2 -5- Eq. 3 (5) LOSSES The most efficient way of coupling the gener­ ator to the load is through an ideal transformer. The power delivered to the load in that case will be called P0 . A quadripole inserted between the generator and load will transmit a power to the load. The ratio P^/l^ unity. Is less than or equal to The equality holds when the quadripole is an ideal transformer. It is shown (6 ) that in the ideal case, Zt ® ^ VZiZ^* Consider the ratio of powers P^/P0 It is effectively /I*/* Zt /T.f 20 . 9 /^|2 - 'Lh IX*)P o Divide the fraction by E^E^and there results £' | * llT^RprJ * zt The ratio R. /P0 can be defined - Power Insertion Ratio *j2 V zlz2 Y t| a 6 Mason, w. P. Eq* ^ Electromechanical Filters and Wave Transducers 1st Edition 1942 New York: D. Van Nostrand. p24 -6- In the study of four terminal networks, Insertion Ratio is often considered. the This ratio compares the current that would flow in the load due to ideal transformer coupling, to the current that actually flows when the quadripole is inserted between generator and load Impedances. It can be evaluated, as follows: This is the Insertion Loss Ratio * . Bode (7) prefers to deal with the inverse ratio, He defines © - log A and B are respectively the transfer loss and the transfer phase. Bode does not use the absolute values in the ratio of currents but treats the currents, and the ratio, as complex numbers. of a complex number Z )Q However, is given by log the logarithm |Zi-*■ JO. Thus, if one takes the reciprocal of the Insertion Loss Ratio, and then takes the natural logarithm of this new ratio, Ibid 3 the Transfer Loss is obtained. P. 73 -7- Consider Y t . Yt = 0 t ^ 3Bt , Yt G t - JBt , . Then |Yt\ - (0t* ♦ ) Y This result will be used later in this thesis in a method suggested by Bode. 7 Bode, Ibid 7 H. E. Network Analysis and Feedback Amplifier Design 19^5 New York: D. Van Nostrand P. 230 (6 ) R-C QUADRIPOLES The essential features of R-C dipoles and quadripoles have been established by Cauer (8 ), and only the points of interest to this thesis are presented h e r e . The driving-point immittances*of R-C Networks are rational functions of the complex frequency var­ iable P- J w . Poles and zeros are simple, real, and i nterlaced. The immittances can be expanded into partial f ractions: n , * Z(p)^a Caf) + P ( a P + Pw K ^ 1 Eq. 7 n , v Y(p) = b < .p + b (uJ ^ p. J 1 where all the a a n d b^ b p + ^ Eq. 8 are positive. These expansions lead to the two canonic forms developed by Cauer for R-C networks, figure 3- 8 Cauer, E. Die Verwirklichung von Wechselstromwiderstanden vorgeschriebener Frequenzahabhangigkeit. Archlv F. Electrotechnik, vol. 17 P355 1927 * Ibid 7 P . 15 -9- o (•ai l/aM i /WWXA— —J| (Impedance Form) Figure 3 (Admittance Form) Canonic Forms of R-C Networks. -10- Quadripole properties are found by insert­ ing the partial fraction expansions, Eq. 7 and Eq. 8 , into the general equation 1 and 2. The terms a r e : z.. = a n 2/i * + 7 p ^ix p ^ p^ 1 r—j * K -P * *>„ + p. n xr> <:v b /7 P + Qv n b/z ■ P -V b ,2 p . 2 1 btrv P -► The very important Residue Theorem0 states: it CM ^ _ vV) i j a« - 0, a 2i i 0 , aM .aijt ~(a,^ ) i: 0 0, for all r . b j '1i 0 , b„ ^ i 2 > ^21 ’ 1S ^ en P ° ssit)l e synthesize the network in any suitable form. Guillemin ° shows that the residue condition is Identical to the realization condition of a symmetrical lattice, in any form, o so If the network is realizable it is always realizable Ibid 7, p. 243 Ibid 9 Ibid 3, P. 381 -15- in the lattice form. other forms, This does not rule out but assures the existance of at least one form, the lattice structure. The lattice will have arms: YB - y ll ' y 12 .E q * 11 12 Y A " y ll Orchard then extracts equal resistances from the lattice arms to act as generator and load resistances. The result appears as figure 5. | Uri — f+ z *\ 4 Figure 5 Extraction of Terminating Resistors The fact that the generator and load resistances are equal is a design limitation of the method. - 16- (8 ) APPROXIMATION PROCEDURE This thesis uses a modification of a device of Guillemin ° to approximate a frequency response. F(w) is given graphically over the complete range --»> < uj s «o A change of variable ux* tan ©/2 changes the range to -it i & s tt t and the F (saO is trans­ formed into a periodic function of ©. is then approximated by Fourier Series. transformation, x the 1 - o* Another -= cos © , changes the series to a polynomial in x , F(x). ation, x This F(^) The last transform­ , returns the approximation to plane. The closeness of this approximation is deter­ mined by the nearness of the Fourier Series approx­ imation to the prescribed F(0). There are many classes of functions that can be approximated by Fourier Series in an arbitrarily close manner, and if the F(®) falls into one of these classes, the approximation will be as close as desired. The mathematical expression that results from the above manipulation Is not in a form suitable for R-C networks. poles. ° Ibid 11 The denominator would lead to multiple In this thesis the approximate P ^ ) divided by a function of will be that is very close to unity over the range of ^ . The choice of this dividing function will be made to clear the denominator. There is liberty in choosing this function, as long as the choice does not change the final result to a point that the approximation is not as close as desired. - 18- (19) APPROXIMATION E X A M P L E . ...LOW PASS FILTER The graphical representation or the desired filter is given in figure 6 . The filter characteristic has been given In terms of lYTj* has been shown to be propor­ tional to the power insertion ratio. (Eq. 4) For the sake of simplicity the graph as been normalized with respect to frequency and m a g ­ nitude. The first change ^ = tan e/2 results In the F(e) as shown In figure 6b. There Is no difficulty in approximating figure 6b, by Fourier Series. Since F(©) is continuous and of bounded variation, a Fourier Theorem (12) states that the series converges uniformly to F(0). By standard methods the first few terms of the series are.... F(0 - .500 - .635 cos© -.204 cos3© +.1215 cos 50 Eq. 11 Since only a few terms will be used, the above approx­ imation might become negative for some 6 . allowable for this is not |YTix > so a different form is used. F(©)- B_+.635 cos©-.204 cos 3© +.1215 cos50 Eq. 12 B^ Is chosen large enough to keep F(©) positive. 12 Churchill, R. V. Fourier Series and Boundary Value Problems. 1941 New York: McGraw-Hill p .86 -19- At O = "ir/2, which corresponds to ^-=-1, the value of F(©)- or \Yr (©)I2- - B — M ake the transformation x ~ cos Q . Then . 3 ^ *■ cos 3© * 4x - 3x# cos 5© l6x - 20x ■* 5x The approximation then becomes: l^x)]1 r ,6 35x 3- .8l6x ♦ .6l2x «.1.944af -2.43x%.6o75x-* • 1.944x*’- 3 . 2 4 6 / + 1.8545x ♦ B - Eq. 12 F o r some value of x, and some ^ , the reaches a minimum. the lYr (^)i* |Yr(x)l* If this minimum is fixed at zero, will not be qero at *•»* •« . This is the result of using too few terms in the Fourier Series. Figure 7 compares the approximation to the F(©). The Inclusion of additional cosine terms would improve the approximation, but increase the work In the computation. Themlnlmum Is found by differentiating Eq. 12. d iYt( X )]* - 9.720x* - 9 . 7 3 8 x ^ 1 . 8 5 4 5 * 0 Eq. 13 x This is a quadratic in x , roots 9 . 7 3 8 * 4.972 197440 The root of interest is x 2 a .245164, x s. .495 At this value of x, B^jnust be .5823278 to have CALCULATIONS FOR GRAPHS © 0 10 20 3° 40 50 60 1° 80 90 100 (Figures 6 & 7) Cos 0 .635 Cos 0 .204 Cos 3© .1215 Cos 5© - .033 Cos 70 1.0 0.9848 0 .9397 0 •866 0.766 0.6428 0.500 0.342 0.1736 0 -.1736 .635 .625 .596 .55 .485 .408 .317 .217 .110 0 -.11 -.204 -.177 -.102 0 . 102 .177 .204 .177 .102 0 .1215 .073 -.0215 -.105 -.144 -.04l6 .0607 .1195 .093 0 -.083 -.0284 .0645 .072 -.0144 -.0816 -.041 .0534 .078 0 .078 ■ — --------- ------------------- --— From 90 to 180 repeat opposite in sign. 0 3 term siim 4 term sum Corresponding U) 0 10 20 3° 40 50 60 70 80 90 100 HO 120 130 140 150 160 170 180 .5525 .521 .4725 .445 .473 .5434 .5827 .5135 .305 0 -.305 -.5135 -.5827 -.5434 -.473 -.445 -.4725 -.521 -.5525 .4695 .4926 .5370 .517 .484 .4618 .5417 .5669 .383 0 -.383 -.5669 -.5417 -.4618 -.484 -.517 -.5370 -.4926 -.4695 0 .087 .176 .268 .364 .466 .577 .700 .839 1.0 1.19 1.428 1.732 2.144 2.747 3.732 5.6713 11.430 -21- The graphs are even functions ofu> P (w)s F(-to). . Then The graphs could he shown to he symmetric In oo ahout the origin, hut only posi­ tive to is of interest. This leads to: |YT (x)Jx s 1.944x* -3.246x * 1 .8545x 4 .5823278 The next change of variable x, 1 - to* 1 r la* Eq.l4 gives 1YT («)(*» 1 .944(1-to* )f-3.246 (1 -co* )(lr co1^ ! .8545(1- & )(!**>* Wfrll + q?*) (1 + w l .- J, Eq.15 Multiplication and binomial expansion puts the coefficients in a form expressed in the tables below: * CO 10 2 2 CO 1.944 -1 3.246 1 1.8545 -1 5 -1 -3 -10 -2 -2 1 CO -5 1 3 Cjo 1 -1 1 This gives: 6o’° -1.944 3.246 -1.8545 CO coa 19.44 6.492 3.709 -9.720 3.246 5.5635 CO* 9 .720 -3 .246 -5 .5635 -19.44 -6.492 -3.709 CO* 1.944 -3.246 1.8545 The numerator is then formed: (B„- .5525)* + • • • • . . .(1 OB *►29.641) to* + (5B«» + .9105 )CO*" 4 (B^t.5525) Wh e n the assigned value for B„ is inserted (B^ *.58 2 3278 ) in the above, there results: .029827740 + 3.8221394?*- 23.817722 u>*+ 3 5 .464278co*4 2.00113940*+ 1 .1 3 4 8 2 . - 22- s Remove a factor of .0298277 and there is formed: l^r (u )|* . .0298277(m'% 128.1 Kg -7 9 8 .5a)*. 11.89.71 u -1 . . ■ .67.089908 u>L* 38.046 Eq. 16 To get In a form for R-C synthesis, divide the above fraction by C(co*). C (Coz) = ( » .81 )(o3fct .9 0 2 )(a>1^ 1 )(coS 1.02 )(0)1* 1 .2 1 ) i V t 1 )*■ There is a little latitude in the choice of C(u>t), and the above form is chosen for the ease in subse­ quent calculations. A table of values for C(Co*) shows that the choice of this expression is close to unity for all oj . 1 CO1 0 c (00l) .9742 .99952 cox 5 C (A)1) 1.00261 1.5 1.0016 2 31 1.0024 1.00288 . 1.0 The divisions of Eq. 16 by C(co4) leaves as a final result: lY, (c*)j . ( . 0 2 9 8 2 7 7 X u A 1 2 8 . 14/ - 7 9 8 . 5 0 6 ^ 1 1 8 9 . 710J.V n — .H I T T — .£627( " 1 .Oc!) ( 1 T 2 I ) --6 7 .0 8 9 6 8 6 ) A P P R O X \MAT\OA/ - 3 T E R M S a 1 2 A/) A p p p Q x IAl fiT/pup S (10) SYNTHESIS PROCEDURE The next step is to synthesize a network that is characterized by equation 17. The numerator of the expression is a polynomial of fifth order in to*. must be found. The roots of the polynomial One root is already known for the |yt (fc*))4, was chosen to have a minimum of zero. This m i n i m u m occurred at x » .495 which is u>*=3.04 5 8 7 8 . An examination of the polynomial shows that there are two changes of sign. rules is applied (13)- One of Descartes This rule states that there will be either two or no positive roots for the poly­ nomial. There Is assuredly one root, and the expres­ sion does not cross the axis in more than one place on the graph. Thus there is a double root at cor -- 3.045878. To find the rest of the roots, the method of Lin (14) is employed. The result is: l*T (-)i'* .0298277 ( - 3 . OA59 ) (<**. 134.158 )(to* *. 07375 J- * ■03056783 ) ( { cjt<■.902 )ecu'*♦ ljlto1* 1 .0 2 )C^*f IT2 1 ) _ Eq. 18 13 Pipes, Louis A. Applied Mathematics for Engin­ eers and Physicists. 14 p.98, 1946 New York: McGraw Lin, S. N. Method of Successive Approximations of Evaluating the Real and Complex Roots of Cubic and Higher Order Equations. Jour. Ma t h and P h y s . Vol. 20. No. 3 Aug. 1941 -24- The synthesis problem requires the Yr (p) so since p - JOB*.nvt> JO - . i 7 V 8 W ) L c p - . « ? ; r p - (P+ /Jcp CP-/-'J Fo r R-C synthesis only the poles in the left This restricts the denomin­ ator to Just the positive factors. There are no restrictions on the zeros of Y^-(p) so there is m u c h liberty in choosing the numerator of the expression. At this stage, G u i l l e m i n ’s method would require the selection of a numerator that would make Yf a m i n i m u m phase shift function. -25- 1 J Eq. 20 half plane can be used. J Lattice synthesis does not required a minimum phase shift function, but for simplicity in this example, and the material following this example, a m i n i m u m phase shift structure is chosen. The graph of | Y T (“Ol^ vs , in figure 6, has been normalized with respect to magnitude. M u l t i p l y the expressions for |YT (di»J* tor Al by the fac­ to represent the unnormalized expression. The significance of this factor becomes apparent when the full equation for Y T (p) is considered. Y-r(p) - 1 Pl t 2 PoYRjRg The above is an extension of equation 4. The m i n i m u m phase shift structure is then: Yt(p). .17271 A(P S , 2 ^ 5 88J0>tl1 52 H p \ .6507P * 1748441 ( p J ; § U p t . 9 5 M P + l ) C p + i . o 5 M P t l.lj Eq. 21 A cutoff frequency (represented by CO* ) could be introduced here. of co This requires the replacement in equation 18 by Coy/(jt)o. W h e n that is done the expression for is found to be Yr (p) 71 A .1727: : p r *. 1 2 .2327P 6J.1- 1 0 . 7 5 7 P t f ^ 3 9 . 2 2 0 6 p V + 23 .4 8 7 p ^ % 6 .1 6 8 0 3 & r_ 5 p V 9 - W 5 p ^ 9 87525X? Eq. 22 - 26 - One form of a complete problem would specify the generator and the load resistances. The required cutoff frequency would also be given. For the purpose of demonstration, let: - R^ - 100 ohms 2 -r 2 Let .......then » 200 ohms. » 1,000,000 rads / sec. The value of A cannot be arbitrarily stated when the impedances and the cutoff frequency are fixed. This will become evident as the problem is solved. The first step is to expand equation 22 by partial fractions. At p - 0, the residue of the right side of equation 22 is equal to 6 .2 4 5 9 5 6 9 . This residue is subtracted from the expression and partial frac­ tion expansion is continued. The details of this expansion are not repeated at this point. The expanded y-, p s 1 (p) - y 12 ls: .17271 A ^6.24596 - 121,418 p (p + L -895,069 p u/o {9 + U/a 657,443 p T * O/0 (p + 1 -0^,) ,560,039 P ... joJq Kv •$5u/o ) + -180,427 p ^p + 1 Eq. 23 -27- Wh e n all the terms in the previous expressions are made positive, the equations for y ^ obtained. « They are: y ll * y 2 2 ‘* •1 7271 A] 6.24596 +121,4l8 p ^ I p t»9 cag / + 89^069 60*^P y 22 are p ■+ 00* ) _ ^ 651>44^p <300 tp ^ 560,039 P cSt (p +• „ _ l 8 o A4 27 P + I.O 50O0) 60*(p «- l.lOJo) Eq. 24 The lattice arms can now be formed. yH * y !2 11 y 12 y a *.17271 A [l2.491 9+ 1,120,078 p 1,314,886 p Lu>0 (p ♦. 9$ c00) 6 0 0 \P + I.0 5 < 50«) “ * Eq. 25 _ Yb * .17271 A 242,836 p + W,lP+-9«»; 1 ,790,136 p .Mo I P « 4 ) 360,854 p L. J Eq. 26 The reciprocals are taken in order to write the arm impedances. A The result is: p r 64112.4^19 P ( 44.'5532*,/ j CO,IP . 1-lcJ,) + 2,5l6>6bo^) «*■ . . 2,455,224^.') 12.454 ) Z_ 3 £J.-t- 2.99V»P + -99 »o3 )__ 5 .79005 ^ A" %,S^3,B28p£ . 4,775,856^ p . 2 , 3 6 4 , 1 . 2 2 ^ p Eq. 27 - 28- These ape driving point impedance expressions Tor the arms of the lattice. At this point these expressions could undergo partial fraction expan­ sion and be synthesized. This would defeat the purpose of the problem for the generator and load resistors would be absorbed in the network. A standard theorem 4 of lattice networks states that if an impedance is common to both arms of a lattice, it can be removed from the lattice and placed in series before and after the new lattice. This theorem is utilized by finding the mini­ m u m value of both arms impedance. Obviously since these are R-C arms the minimum impedance occurs when f » •• Z p -* — „ __ 5.72 0Q5a__£0* . A (12.4919 2,515,656) . lim Zn P - . T then 5.79005 coo “ A (2,393VBBS)------ Eq. 28 The smaller of these two limits is the first. Then a resistance equal in magnitude to the first part of equation 28 is common to both lattice arms. This m i n i m u m resistance can be removed from the lattice. Ibid 7, p. 269 -29- Tills m i n imum r e s istance, designated as Z* , Is obviously the generator and load resistance. If the Z' turns out to be larger than the desired resistances, only the needed amount need be pulled from the lattice arms. In the assigned problem, Z* should equal 100. Z 1 •> 5.79005 GOo AU2.'*919ofc+2,5l5,bfc>t>; F o r the a s s i g n e d o f of A is _ 100 ohms 1,000,000, the derived value A m 0.003858078 W h e n this value of A is know, it is inform­ ative to solve for the Power Insertion Ratio. At p = 0, the equation 18 leads to \*T (p)lp.e A 1 ( . 0 2 ^ ^ ) ^ . 0 ^ ^ 4 . ^ a i (_ 2 325§Z§al. - B u t tYt (p)j* ' A 2" (.4 1 3 1 8 6 1 7 ) . 4 p 2_____ R-jRg s P t, (40,000) z A* ( .41318617) Thus at zero frequency the Power Insertion Ratio is found to be PL P* _ .24600598 F r o m the graph the ratio of Maximum IYt (^)i* |Yt (O j*. is about 1.08/1 so the maximum Power Insertion Ratio is about .2 6 5 . -30- This is a result that is not evident from a cursory examination of the problem. It is now seen that for a given load and generator resis­ tance, and a specified cutoff frequency, the max­ imum allowable Power Insertion Ratio is automat­ ically determined. If it had been required to find a filter with the same load and frequency requirements as the previous problem, but with a higher Power Insertion Ratio, some other form of synthesis would be required. Such a filter as the latter is not realizable by the method just utilized. It Is quite possible that there Is no R-C structure that will satisfy a requirement of a higher Power Insertion Ratio. This subject requires further investigation. The filter problem can now be completed. 100 ohms, or Z*, is to be subtracted from ZA and Zg. The modified lattice arms Z^ and ZB * are now com­ puted . With numerical values the arms are: Z . .1500.76( p* + 2x10 S? 15 .0075bbp* Zo * » ♦ .997x1Q 12, ) * 24.9 8 3 x 1 0 *p «- 12.454 1500.76 (p* » 3x10%***. 2.99xlOa p » .99x10>g) 2.39382p 4 .7 7 5 ^ 5 * 1 0 iP 1- + 2 364 ,122x10* p ) Eq. 30 -31- W h e n lOO is subtracted from equations 30, the modified arms are obtained. _ 1503.22xl0*p + 1.4962577x10 '*______ Z » 15.0075bbpr + Z_» 2 4 !963x 1 0 Jp + 1 2 .4^4 _ 1 2 6 1 .38ps - 4027.xl0*p *■ + 4250.86x10/2'p .*.l485.75x 2.5S38£p> +-*7775,U50pi + 2 , ^ 4 , 1 -2 2 x 1 6 ^ --- B Eq. 31 The usual methods of partial fraction expan­ sion are then used to realize these driving point impedances. F o r the first case the impedance is simpli­ fied by dividing numerator and denominator by 15 .007566 . V A ■ 99.7H7*1Q*P,,t £> •°997glO 1 ,6 6 4 , 7 4 7 p .8 2 9 twa 99-7117x10 * p * .0997x10 ,s — Ip 7176647747 )( p T T G r ) Eq. 32 Equa t i o n 32 is expanded by partial fractions. The result is: Z.« A (5.98889 )xlO/0 a ( p V 3.98227x106 0 1 ) -------- P / I . 5 6 4 7 5 0 0 r - Eq. 33 This driving point impedance is represented by the figure 8 . -32- R^A » 5.989x10^ ohms « 2a " ohms C-jA * 16.6975 CgA =* 0.251113 uufd ufd Figure 8 >^2/1 j w w l __ \a a a I— (f--1 Cl A 1— I C 2.A Lattice Arm Z* A very similar manipulation is done Tor the other lattice arm. The numerical calcula­ tions are a bit more complex, because the denom­ inator os the expression is a cubic polynomial. Luckily, one of the roots of this denom­ inator is at p s 0. This simplifies the cubic solution to the solution of a quadratic. The expression for Zg» is found in equation 31. D i v i d e both numerator and denominator by 2.39382 and there is obtained as the driving point impedance of the lattice arm: 2= * . 526 .931pJ 1 6 8 2 .2xlOfc p\. 1 7 7 5 .77x 1 0 '* p+6 2 0 .66x l 0*8 ^ p C p * ■;l,995,674p 875,933x10 * T ------------Eq. 34 There is no great difficulty in obtaining the roots of the denominator by the quadratic f o r ­ mula. The roots are: - 1,084,063; - 911,010.8; -33- 0. The partial fraction expansion, when applied to Zq * gives the following results zB * « 6 2 8 .4 5 7 p ^ 6 1 ,2 5 3 .1 5 0 p + 1,084,063 „ 5 8 3 ,6 3 6 P + 91T 70T 0 Eq. 35 The realization of equation 3 5 , which repre­ sents the lattice arm — H V is shown in figure 9 . M/V. ... ' — ^ * ----- 1 1 ------ ---- H | ---- 1 C IB 5 LB Figure 9 Lattice Arm Zg* The numerical values for the components are: C nR ■ 0.00159 farads C 9p * O.OI63 farads R 1B s 56.50 ohms s 1.713^ farads Rpr _.0.6406 ohms The complete lattice formation is shown in figure 10. The quadripole realized in this problem for­ tunately requires the use of components that are available in a laboratory. -34- A less fortunate choice of cutoff frequency, or of terminal Impedances could have led to capacitors in the order of farads, not ^ f a r a d s ; the result might also have required m i c rohm resistors. If that were to be the case, another method of R-C synthesis not in the form of a lattice, would be in order F o r that reason, a high cutoff frequency was chosen for the demonstration problem. C»* CzA C,B IB '33 Lattice Arm A Lattice Arm B Ri« ■ 5 . 9 ^ 9 x 1 Ohms R IB - 56.50 Ohms R*.* Rt,® * 0 .6406 Ohms s 2 .3921 Ohms Cj*)* 16.698 Cj a s 0.2511 farads Cj s - 0.00159 4t farads Cjg = O.OI63 44 farads Gse- 1.713^ 4f farads ^farads Terminal Resistors Rf % 100 Ohms R£ 100 Ohms = Figure 10 Final Lattice Structure -36 - (11) REALIZABILITY OF A QUADRIPOLE A glance at figure 7 shows that the synthe­ sized lattice has a frequency response that merely approximates the desired trapezoidal pattern. This is due to the fact that only a few term of the Fourier Series were used. The inclusion of additional terms would bring the response of the filter mor e like the desired characteristic, but the inclusion of more terms would require more com­ plex calculation and require the addition of ad d i ­ tional circuit components to the lattice. Since the desire F (9) is a continuous func­ tion, it was stated before, that the desired res­ ponse could be approximated arbitrarily close. A F o u rier Theorem® states that if F (9) satisfies these conditions: F(0) * F(©+2 tt) for all 9, and F(9) is sectionally continuous in interval (—/r, tt), then the Fourier Series converges to the value £^F ( d * ) t P ( O' )] at every point where F(0) has a left and right hand derivative. The trapedoidal pattern fulfills these r e ­ quirements^ so an infinite number of terms could result in a theoretics expression that exactly realizes the desired response. Ibid (f2) p. 70 -37- (12) E X T E N S I O N TO THEORY OF EQUALIZERS. Consider the system shown In block diagram form in figure 11. In this system, a signal passes through a Low Pass Filter. Some of this signal is utilized in the filtered form, and the rest of the signal is isolated by a vacuum tube and sent on to an Equalizer. Since the filtered signal passed through a Low Pass Filter, the Equalizer must be a Hig h Pass Filter. A system such as this can be handled by the methods of this thesis, for the problem of the interaction between the High Pass and the Low Pass F i l t e r is solved by the use of the Isolation A mpli­ fier. The system requirement might be that the product of the Power Insertion Ratios of the High and Low Pass Filters be a constant; or the require­ m en t might be that the sum of the ratios be a con­ stant, for all to . The characteristic required for the High Pass Filter can then be transformed Into a Fourier Polynomial and the synthesis performed. -38- SIGNAL LOW PASS FILTER FILTERED SIGNAL * ISOLATION AMPLIFIER EQUALIZING HIGH PASS FILTER | Figure 11 4 — EQUALIZED SIGNAL Block System using Equalization -39- (13) HIGH PASS FILTER SYNTHESIS It Is desired to synthesize a High Pass Filter such that the sum of the Power Insertion Ratio of this filter and the filter previously designed in this thesis be a constant for all. The Power Insertion Ratio characteristic desired for this filter is shown in figure 12. The Fourier representation for this filter is readily obtainable from the Fourier represen­ tation of the Low Pass Filter, equation 36. The expression for the High Pass Filter is obtained when the Low Pass characteristic is sub­ tracted from its maximum value. Thus, unity, if equation 18 were subtracted from the result would be: .0 2 9 8 2 7 7 (