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