Robust time-Optimal Control for Flexible Structure Vibration Control by Augmented Dynamics

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Robust optimal control problem for flexible spacecraft/structures using on-off type discrete actuators has been a subject of intensive research. Optimization by switching time parameterization can be used to minimize the maneuver time subject to equality.
Publisher
한국항공우주학회
Issue Date
2004-05
Language
English
Citation

INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.5, no.1, pp.19 - 29

ISSN
1229-962
DOI
10.5139/IJASS.2004.5.1.019
URI
http://hdl.handle.net/10203/228696
Appears in Collection
AE-Journal Papers(저널논문)
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