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
Link To Document :
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