NDLI: Algorithms of control for precise stabilization, orientation and manoeuvres of spacecraft

Content Provider	IEEE Xplore Digital Library
Author	Arumov, G.P. Frolov, V.A. Sidorov, I.M.
Copyright Year	1998
Description	Author affiliation: Space Res. Inst., Moscow, Russia (Arumov, G.P.)
Abstract	For the solution of orientation and stabilization problems of dynamically complicated spacecraft with random external interference, a model-based control method is described. The main idea of the method is that at a given time interval the coordinates of "sample" motion (the flexibility is absent) and the oscillations of flexible and mobile elements of the construction are defined separately. On that basis the results of motion analysis allow one to identify the random interference and oscillations with subsequent changes of structure and parameters of the algorithm and to provide precision orientation, stabilization and manoeuvring. This method with elements of identification and adaptation allows one to reach a much higher accuracy then the widely used Kalman filter method. The algorithm has high stability towards considerable deviations of model's parameters from the nominal values.
Starting Page	4392
Ending Page	4395
File Size	340118
Page Count	4
File Format	PDF
ISBN	0780347781
ISSN	1062922X
DOI	10.1109/ICSMC.1998.727540
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	1998-10-14
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Space vehicles Control systems Automatic control Interference Motion analysis Stability Frequency Aircraft navigation Accelerometers Object detection
Content Type	Text
Resource Type	Article

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