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1 FOREIGN TECHNOLOGY DIVISION o~ I14 fapplication OF THE METHOD OF HARMIONIC LINEARIZATION FOR I INVESTIGATING SLIP MODES IN A DIGITAL TRACKING SYSTEM WITH VARIABLE STRUCTURE Ye.Ya. Ivanchenko, V.A. Kamenev JAN A Approved for public release; distribution unlimited. 92 0

2 FTD -II)(RS)T EDITED TRANSLATION FTD-ID(RS)T December 1981 MICROFICHE NR: FTD-81-C APPLICATION OF THE METHOD OF HARMONIC LINEARIZATION FOR INVESTIGATING SLIP MODES IN A DIGITAL TRACKING SYSTEM WITH VARIABLE STRUCTURE By: Ye.Ya. Ivanchenko, V.A. Kamenev English pages: 9 Source: Izvestiya Vysshikh Uchebnykh Zavedeniy, Elektromekhanika, Nr. 6, 1971, pp Country of origin: USSR Translated by: Robert D. Hill Requester: AFWAL/FIGL rarc sr on -or Approved for public release; distribution unlimited. el D ~~istrib.on Ava iltt Codes Dli l Special THIS TRANSLATION IS A RENDITION OF THE ORIGI. HAL FOREIGN TEXT WITHOUT ANY ANALYTICAL OR EDITORIAL COMMENT. STATEMENTS OR THEORIES PREPARED BY: ADVOCATED ORIMPLIEDARETHOSEOFTHE SOURCE ANDDO NOT NECESSARILY REFLECT THE POSITION TRANSLATION DIVISION OR OPINION OF THE FOREIGN TECHNOLOGY DI. FOREIGN TECHNOLOGY DIVISION VISION. WP.AFB. OHIO.. FTD-D( RS)T Date 4 Doc 19 81

3 " -"U. S. BO0ARD ON GEOGRAPHIC NAMES TRANSLITERATION SYSTEM r;block Italic Transliteration Block' Italic Transliteratic,. :A e i- A a A, a p p Pp Rý r b bo 5 6 B, b -C C C C S s SB V, v T T D,a dp 0F) T Pp m Tj aac Fr- r e G, g Y y Yy U Su E e E ' Ye, ye; E, e* X x X x Kh, kh m M Zh, zh Q LA Ts, ts 333 Z.z q t. Ch, ch 11 Sy,, IW y A Wi LU zq am Sh, Shch, sh shch K JC x K, k b ".J7,1U W hl V a Y, y "MM M.m m & HH H Hi N, n 9 Ee 0 o 0o O, 00 o A0 w Yu, yu L n n 17 n P, p H A R x Ya, ya * ye initially, after vowels, and after 6., b; e elsewhere. When written as 6 in Russian, transliterate as y! or. RUSSIAN AND ENCLISH TRIGONOMETRIC FUNCTIONS Russian English Russian English Russian Engli -ý. sin sin sh sinh arc sh sinh- Cos Cos ch cosh arc ch coshtg tan th tanh arc th tann. ctg cot cth coth arc cth cothsec sec sch sech arc sch sech cosec csc csch csch arc csch csch Russian rot lg English curl log r 77 ; o

4 APPLICATION OF THIE METHOD OF HARMONIC LINEARIZATION FOR INVESTIGATING SLIP MODES IN A DIGITAL TRACKING SYSTEM WITH VARIABLE STRUCTURE i Ye.Ya. Ivanchenko, V.A. Kamenev t At the present there are not any accurate methods for solving I a nonlinear differential equation of any order. Therefore, used very I frequently are approximation methods to study nonlinear control sys-!,tems, which allow obtaining results with an accuracy sufficient for Iipractice. In --...I I L. -- I the proposedwork the problem is stated concerning the ".'..... application of the widely known method of harmonic linearization of Ye.P. Popov for investigating slip methods in structure (SPS). a system with variable S~A very important characteristic of the SPS's is the fact that Sthey allow ensuring a high-quality control of the free movement of S~objects with constant parameters, and in the case of a change in the parameters of an object over a wide range they allow constructing a Ssystem which is barely sensitive to these changes. In reference [1] a detailed description is given of the principle of constructioi of the SPS, and methods of the phase plane are widely used. Problems of harmonic linearization and frequency methods of the investigation of the SPS are examined in references [2], [3] and i Let us examine the digital tracking system with variable structure (TsSS SPS) in th~e control of pit-shaft hoisting machines along a track. Let us take the closed and opened structures as the initial. structures. The component (Fig. 1 connected to the input of thei

5 control system, serves as the element for switching of the structure. The logical law of. switching: of the structure has the form when..-., N' px) when,x.(' 0 )i11 where F(x, px) is the nonlinear function; x - the output value.,j I UX ýj,, 4 Fig. 1. Block diagram of the switching element: vj, j acting and assigned rates of movment; h. x 3 traversed and assigned paths of movement. Key: 1) Rate comparison circuit; 2) Coincidence circuit; 3) Error signal of track; 4) Comparison circuit of track*; 5) "greater"; 6) "less." [Translator's note:*track and path are used for the same word in the Russian.) Since the element for switching of the structure is connected at the output of the digital-analog (Ts-A) converter of the register of the matching of the track [path], then the statistical characteristic and also the input and output signals of the combined nonlinear element (element of switching of the structure + converter Ts-A), in the presence of a constant and slowly changing shift in x, will have the form depicted on Fig. 2. In this case, with the expansion of the nonlinear function F(x, px) in Fourier series, there appears the slowly changing constant component, owing to which the harmonic linearization of nonlinearity takes such a form [5) j higher harmonics, where x, px) =,,, + a~x,, 3)x*+ A. x 0.,7) 1'' PXpx* *+ + Is r \-(x" -2Asin?, 2 A-acos

6 ,i.-. I-',- /"IX' A sitip, Awcos?)sli's id ; (i) " xt. 4 A si?, A.cos?)cos d?, (5p)d, x* is the self-oscillating component with a slowly.changing amplitude and frequency t) ; a _arcsihs - switching angle of the structure; - A A - - amplitude of the Input signal; S -quantization increment. UX I'1 Fig. 2. Statistical characteristic and nature of the input and output signals in the SPS with the Ts-A converter. If '.e consider that at the moments of dimens;ionless time o'4 and,'f the output function F(x, px) by a jump increases by one, and at moments 13; and 4i by a jump is decreased by one, and at other time values it r ls constant and wit!, a change in the angle from PO to 7r and from ý0 to 2?r is equal to 0, then the coefficients of harmonic linearization F 0, a and b, computed from formulas (3), (4) and (5), have the form 2i-l 2i-1 - I z I 2- (6)

7 (2si_2 "[ ln2 X(7) I' b si- n), (8) where i is the integer of steps of the characteristic; k - maximal number of steps of the characteristic covered by the input signal. For the TsSS of the shaft-pit hoist hoisting machine, the multistep characteristic can be reduced to a relay by applying the variable quantization increment [6]. By keeping this condition in mind and knowing that in the slip mode the control action of the relay element is a sequence of pulse of one sign [7), let us write conditions of the existence of the slip mode for one quantization increment. Since the condition of operation in one direction has the form A 1-0,5 0,5 - x, (9) and the condition of the absence of operation in the other direction and in the direction of the change in the quantum is IX l. -.O..) > A. -. ec, if i 0xl,. 5,,I 1,5--XI" :> -If's I~irS, o.,,., I.,o, O e'~ i 1x1'.~ }(10) then the condition of the existence of the slip mode denotes the combined fulfillment of conditions (9) and (10). Taking conditions (9) and (10) into account, coefficients of harmonic linearization for the relay characteristic 1) in the j slip mode will take the form t. 0.n -2:ircsin ) - Atl -C s2)i: (11) 2 ~I,sin2,, By representing the slip movement as a slow change in the coordinate and the pulsations imposed on it, changinl and periodic components. we will distinguish the slowly Then instead of one harmonically linearized equation, we will obtain two kinds, respectively, for the - 4

8 s;lowly changirg aind self-oscillating components of' the slip movement,j (/,).r. i N ')f* I p:% -XP(a:~. + r f to li where L(p), N(p) and S(p) are polynomials, and f(t) is the external disturbance. To find the periodic solution, let us examine the second equation of system (14). The differential equation of the TsSS SPS by the pit-shaft hoist for the self-oscillating component will have the form where coefficients A =a, A2 Vhl ; A.,=O,0Sa,': A 4 satisfy the criterion of optimal figure of merit [6); a 1 =-;y, - "p the time factor; 1. - calculated duration of the transient process. Having substituted p 1j' into equation (15), let us select the real and imaginary parts and equate them to zero X A, x(, A A,%,A,,2 +-A,,,t+A,-7A, x, 0, ; A, x 1, u), -- A 2-3 4* A 4 A,'b(, U 0. (1 6 ) We will solve the obtained system of equations grapho-analytically. We define the amplification factor A 5 from the the first equation of system (16) I.(A --A,,I A, = (17) To find the amplitude of pulsations A and frequency 0, let use the following method. From the system of equations (16), we find 4.'. - x h,,,, I =Aj,,2-t,,,4- A4 a(a, x to, a) w(a,.-a1=4) (18) us Equation (18) can be solved graphically (Fig. 3). To do this, from requations (12) and (13) we construct in the second quadrant dependences of quantity d on the amplitude of pulsations A for different s;hifts in x when O = const. From equation (12) we plot the dependence of the coefficient of harmonic linearization 4 on the

9 P-I -! 0 amplitude of pul-sations A for different value," of shifts in x0 at the same value of Of, and from eraation (1.8) we plot the cependence of the ratio of d on the frequency of pulsations * W Being assigned values of (;, it is possible for each taken values of ( and x to determine the amplitude of pulsations of harmonic linearization Q/, and then from formula (17) the necessary amplification factors of the TsSS SPS in A and coefficient values of the slip mode are found. The sequence of the determination of A and d, is shown by arrows on Fig. 3, and the dependence of the amplification factor on the amplitude of pulsations, found by the grapho-analytical method described above, is given on Fig. 4.,I th asgnd, -. and - I,,. Fig. 4. Dependence of the amplification S,flctor/ of the TsSS SPS onthe amplitude the G, ~.and ssiged ;.m~[ - -l-, of 0.6 pulsations in the slip mode: Fi 3. Sei u n e oteristic. S-unstable part of the characteristic; stable part of the charac-

10 p.; - ~.,- 1,# S.3- Fig. 5. Smoothed functions of the shift in the nonlinear element for the slowly *--- c, '"'! changing component in the slip mode. In order to determine the slowly changing component F (x ), in equation (11) it is nece.ssary to exclude A, for which we plot the dependerice of the amplitude of pulsations A on the shift in x 0 when A const, having used the graph depicted on Fig. 4, taking condi- 5 L tions (9) and (10) into account. Then, according to formula (11), exluding A, we plot the dependence F 0 (x ). The found functions of the shift in the nonlinear element in the slip mode (when 0( = 0.51r) are given on Fig. 5. After the linearization, the obtained characteristics arc described by equations (when 0.5tr) V'" -- 0,, 5.%' -4 oi,l'] t lip ii A.,,' ',] h lsi /).-,5,... ' (~Jj ~ *. I 19)J~ Figure 6 gives dependences of the amplification factor A* oalculted by the described method, on the curvature of the linearized characteristic of the nonlinear element k for the slowly changing component for different switching angles of the structure 0(. By using the obtained dependences (19) and substituting them, into the first equation of system (14), it is possible to construct by the method of trapezoidal frequency characteristics the transient proces for the slowly changing component in the slip mode both for the con~trolling and disturbing actions. The curve of the transient process for the slowly changing component for the controlling action. when a 0.21Y and A 5 = plotted by the method of trapesoidal frequency characteristics, is given on Fig. 7. Curves of the 7

11 h ] transient process for different values of the amp)i iicatlon factor A can be similarly plotted, 0' " Fig. 6. Dependence of the amplification r,005-i- c'- ik f'actor of the system on the curvature of,17,... the linearized characteristic of the SI I, "k._ nonlinear element. 49 0, /~.,5 kc Fig. 7. Transient process of the TsSSln SPS according to the controlling action. tehere tl i where t is the timec Results of theoretical studies of slip modes of the TsSS SPS were conducted on an electrodynamic modelen. Figure 8 gives an oscillogram of the section of the change in rate from V = 10 mas to V = 0 with constant acceleration for selected values of parameters 0( = 0.21r", A 5 = 0.001a,5 and a 1 = s-i The calculation of parameters of the model is carried out Lccording to the method described in [6]. Operation o the f TsS S Swas con-. ducted in the slip mode with a variable quantization increment. The criterion of the coincidence of results of theoretical and experimental studie ithe s magnitude of error [mismatcht of the path, wrtich, according to the calculations, mustnt exceed the quantlzation to _. the increment method desriedin(6..peaton.f'th.tss...ws.on for any value of the rate. The slip mode, which 8

12 I ~tions consists in oscillations inthe error of' th-ihb mgiueo one quant~um is clearly marked on the occillogram (Fig. 8). Owing to the fact tha~t the traveling quantum is selected aa variable and inacreasing with an increase in the rate, the frequency of the oscilla- is c1~anged insig~nificantly with a change in the rate from maximal to zero, Evident are pulsations of' the slowly changing cornponent, which consist in pulsations of rate. The error with respect to rate is such that the magnitude or' the error of the path does not exceed the quantization increment, which indicates the high-speeda operation of the system of automatic control. I Iin Fig. 8. Oscillogram of the section of slowing down of' the TsSS SPS the slip mode: 1 - assigned rate of movement; 2 -actual rate of movement; 3 -. current; 4i - error of the path. ý_j The proposed method makes it possible, with an accuracy suffi.- cient for practical calculations, to calculate parameters of the slip mode in the digital tracking control system with variable structure, the dynamics of which is described by the nonlinear differential equation of a high order. Submitted initially 28 April 1970 Bibliography after revision 20 Oct. 1970A I' m~ e Ca h R It 0 It C, 11 ClICleMiA 111TOMTIVI.,CCI(JO ynp,%bjiqiiitir C ncp"""t~i CPK 2. )K 1. to fk K.1'ca.0ttII cie- C.101,14'lei:K1111 3I1W.1110 I0 3. X t,a110 it~ It.)I G, CAPt" a~ht K' i twictic %T'j.11OCI,101uIt a,1 WI MITa ~ ~ ja~i P3KT,1141~AM 1O CT11.IIK kmit6 pl twv01e o II a c ca~i c l it*i~ 26 19M, IM 8,~ S. C t ikt i. i.. Au il.otaiciii't H C tl.ct 1IA~ lii V1.4.H4 It UC IIMIIl Ino., liet 9t It.It.. ill... Itelpola, 0.1v. K oif..ii

AO-A FOREIGN TECHNOLOGY.DIV WRIGHT-PATTERSON AFB 0ON F/G 13/7 MEMORY DEVICE U) MAR A2 N A PASHKIN, V N MALYUTIN UNCLASSIFIED FTD-ID(RS)T 0163

AO-A FOREIGN TECHNOLOGY.DIV WRIGHT-PATTERSON AFB 0ON F/G 13/7 MEMORY DEVICE U) MAR A2 N A PASHKIN, V N MALYUTIN UNCLASSIFIED FTD-ID(RS)T 0163 AO-A112 161 FOREIGN TECHNOLOGY.DIV WRIGHT-PATTERSON AFB 0ON F/G 13/7 MEMORY DEVICE U) MAR A2 N A PASHKIN, V N MALYUTIN UNCLASSIFIED FTD-ID(RS)T 0163 82 NL MEEEEM Hfl~ 1.02 0 IIII18 111111.25 RE I TfSTjlR

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