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SCIENTIFIC ABSTRACT YEMELYANOV, S.V. - YEMELYANOV, V.L.

Document Type: 
CREST [1]
Collection: 
Scientific Abstracts [2]
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP86-00513R001962620020-3
Release Decision: 
RIF
Original Classification: 
S
Document Page Count: 
100
Document Creation Date: 
November 2, 2016
Document Release Date: 
March 15, 2001
Sequence Number: 
20
Case Number: 
Publication Date: 
December 31, 1967
Content Type: 
SCIENTIFIC ABSTRACT
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PDF icon CIA-RDP86-00513R001962620020-3.pdf [3]5.78 MB
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. .-, q A - ; I , 11 . ~li a Y I ME19 a L - I- 1 1-2 L4 n e,p, - - , , , jr-)v rl-" -- I I-.1, - ~ li.-- - -, b 19 - - ~ - ~ -1-1 1- - f ~'. __ ~ "t 's ac c MITIt . A PU- -- - - -- - - -.. - - - - - -~ -4x, -,I -.n -:z -I izzt -I Mal, I : I : AVEN, O.A.; DVORETSKIY, V.M.; DOMANITSKIY, S.M.; ZALMANWN, L.A.; KRASSOV, I.M.; KRUG, Ye.K.; TALI, A.A.; KJ1OKJ1DDV, V.A.; BULGAKOV, A.A.; DEMIDENKO, Ye.D.; BERNSHTEYN, S.I.;,AM S.V.; LERNER, A.Ya.; PEYEROV, M.V.; PERELIMAN, I.I. FITSSERI CHELYUSTKIN, A.B.; ZHOZHIKASHVILI, V.A.; 1LIIN', V.A.; AGHhN, D.I.; GUSHCHIN., Yu.V.; KATYS, G.P.; MELITTSER, L.V.; PAqKHOMENKO, P.P.; MIKHAYLOV, N.N.; FITSNER, L.N.; PARKHOMENKO, P.P.; ROZENBLAT, M.A.; SOTSKOV, B.S.; VASILIYEVA, N.P.; PRANGISHVILI, I.V.; POLONNIKOV, D.Ye.; VOROBIYEVA, T.M.; DEKABRUN, I.Ye. Work on the development of systems and principles of automatic control at the Institute of Automatic and Remote Control during 1939-1964. Avtom. i telem. 25 no. 6007-851 Je 164. (MIRA 17:7) ACCESSION NR: AP4041463 SIO 103/64/m/oWoesi /0866 AUTHOR; Yerne yanov, S. V.; Taran, V. A. (Xwftw) TITL~.-, Stabilizing' variable -structure automatic -control system by inertial 7 units th a variable time constant SOURC~: Avtornatika i telernekhanika., v. 25, no. 6, 1964, 861-686 TOPIC TAGS: automatic control, automatic control theory, 'Variable structure automatic control ABSTRACT: In the authors' previous works (referenced in the article), it was shown that instead of using an error-signal derivative, the error signal may be transformed by an inertial (relaxation) unit, the time constant T of the unit being limited by stability and trans iont-response conditions, Shortening the time constant makes the system more sensitive to the variation of parameters of the correcting units. The limitations imposed on T can be alleviated by step-changing CUM I /Z ;ACCESSION NR: AP4041463 the transfer factor of the inertial unit simultaneously with changing the system structure. In the present article, another. correction method is suggested for desensitizing an automatic -control system. This method involves a step-changing of the time constant T of the inertial unit. The dynamics of a second-order free- migrating system is investigated.' The domain of existence and the equation of motion of the sliding mode are considered, as well as conditions of stability and aperiodic motion. The stop -time -constant method is recommended for the case when I - A T > 0 (with high values of A ) Is the f undamental limitation. For the general case$ a switching of both the gain and the inarti&l-unit time constant is recommended. Orig. art. has: 3 figures and 34 formulas. ASSOCIATION: none 'SUBAUTTED: 00 ENCL: 00 '!SUB CODE.- DP,. 1E NO REF SOV; 003 OTHER! 000 C.,d 212 AOCESSION NR: AP4019965 S/0020/64/154/()06/1294/1296 Utkint- AUTHORS: Petrov, B.N. (Academician); Yemql'yanov, S.V.; ;TITLE: Principle for designing invariant automatic control systems with variable structure ;SOUROB: AN SSSR, Doklady*, v. 154, no. 6, 1964, 1294-1296 "TOPIC TAGS: automatic oontrolt automatic control systemg variable ietruature, invariant control systemt low order a9tatism, invarlance ,theory,mathematical determination ABSTRAOT: An attempt was made to make use of some properties of an -automatic control system with a varihble structure for assuring a ~full reproducibility of the controlled coordinate of the manipulated :variable. It was aqsumed that the disturbance and manipulated :variables belong to a sufficiently wide class or functions - a class of polynomlals of anyg but finite, degree of time*. The coatrol ,'.principle should be formulated without a change in the disturbance or some Internal coordinates of the objects. Suppose that the motion ,of an automatic control system In the domain er'of an n-dimenoional ACUESSION VR-- AP4019965 of differential equa- 1 (x1 . ..... xn) is described by the system tione dx M I (K.;, no 7 ,vhere or axt > Oe 1, 2. .(2) f0t Oxi < 0, e are constantso C;C1. it is supposed that the objeetS QuItrol Is realized by an astatio controller with proportional feed- ;back. In that case a are values which axe linearly dependent upon Pf the feedback .kM the coefficient o controller's proportional P M Q, (P) g, (4., 0 (t) - kG (0 + pG I.The domain'U is defined by the relations dx C71>0 :fOiq

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