DocumentCode :
3268761
Title :
Precision gyromoment attitude control systems of rapid manoeuvring spacecrafts for remote sensing and land-survey
Author :
Anshakov, Gennady P. ; Antonov, Yuri G. ; Makarov, Valentin P. ; Matrosov, Vladimir M. ; Somov, Yevgeny I.
Author_Institution :
Cental Specialized Design Bur., Samara, Russia
Volume :
2
fYear :
1994
fDate :
18-21 Oct 1994
Firstpage :
10
Abstract :
Presents results for precision gyromoment attitude control systems (ACSs) for fast-manoeuvring low-orbital remote sensing spacecraft (RSS) with a moment gyrocomplex (MGC) in the form of a minimum-excessive scheme of four gyrodines (GDs) with electromagnetic suspension (EMS) of the rotors. The authors discuss the employment of mathematical models, methods, algorithms and software for their optimization and dynamic investigation
Keywords :
aerospace control; artificial satellites; attitude control; gyroscopes; algorithms; dynamic investigation; electromagnetic suspension; gyrodines; land-survey satellites; minimum-excessive scheme; moment gyrocomplex; optimization; precision gyromoment attitude control systems; rapid manoeuvring spacecrafts; remote sensing stellites; rotors; Aerodynamics; Aerospace industry; Control system synthesis; Employment; Lyapunov method; Mathematical model; Optimization methods; Remote sensing; Space technology; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Satellite Communications, 1994. ICSC'94., Proceedings of International Conference on
Conference_Location :
Moscow
Print_ISBN :
0-7803-2514-1
Type :
conf
DOI :
10.1109/ICSC.1994.523123
Filename :
523123
Link To Document :
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