Abstract This chapter presents the operating modes of a typical modern satellite attitude control system (AOCS). The various modes are presented in terms of functional requirements, H/W architecture, functional block diagram and controller characteristics. The control mode dynamics are described through various simulations.
The AOCS Functions
28.10.2015
67 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
British Library Online Contents | 1997
|NTIS | 1991
|British Library Conference Proceedings | 2003
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|AOCS annual meeting and expo; Virtual 95th AOCS annual meeting & expo
British Library Conference Proceedings | 2004
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