DocumentCode
358080
Title
Parameters synthesis of spacecrafts orientation systems executive units as a multivariable systems
Author
Dmitriev, V.S. ; Gladyshev, G.N. ; Kostuchenko, T.G. ; Vorotnikov, A.S.
Author_Institution
Tomsk Polytech. Inst., Russia
Volume
1
fYear
1999
fDate
1999
Firstpage
343
Abstract
The problem of electromechanical multivariable systems synthesis is considered. The authors give the results of analytical studies on an example of weight and size characteristics optimization of attitude control systems actuators of space vehicles conducted with use of the special software developed for these purpose, with use of a main criterion method
Keywords
actuators; attitude control; multivariable control systems; space vehicles; attitude control systems; electromechanical multivariable systems synthesis; main criterion method; parameters synthesis; size characteristics; spacecrafts orientation systems; weight characteristics; Actuators; Control system synthesis; Electrical equipment industry; Electromechanical systems; Industrial control; MIMO; Optimization methods; Satellites; Space vehicles; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Science and Technology, 1999. KORUS '99. Proceedings. The Third Russian-Korean International Symposium on
Conference_Location
Novosibirsk
Print_ISBN
0-7803-5729-9
Type
conf
DOI
10.1109/KORUS.1999.875940
Filename
875940
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