Adaptive structures for large precision antennas

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Optimal controller design approach for high precision pointing maneuver of flexible spacecraft by using adaptive structures is investigated in this paper. A parameter optimization technique is used to find out controller parameters minimizing a desired objective function which represents pointing performance of a flexible space structure. Multi-input and multi-output configuration used in this study also provides insight on the effectiveness of actuator location for improved performance. Copyright (C) 1996 Elsevier Science Ltd
Publisher
PERGAMON-ELSEVIER SCIENCE LTD
Issue Date
1996-02
Language
English
Article Type
Article
Keywords

LARGE SPACE STRUCTURES; VIBRATION CONTROL; DYNAMICS

Citation

ACTA ASTRONAUTICA, v.38, no.3, pp.175 - 183

ISSN
0094-5765
DOI
10.1016/0094-5765(96)00062-8
URI
http://hdl.handle.net/10203/74464
Appears in Collection
AE-Journal Papers(저널논문)
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