Robust time-Optimal Control for Flexible Structure Vibration Control by Augmented Dynamics
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.
- Issue Date
- 2004-05
- Language
- English
- Citation
International Journal of Aeronautical and Space Sciences, v.5, no.1, pp.19 - 29
- ISSN
- 2093-274X
- Appears in Collection
- AE-Journal Papers(저널논문)
- Files in This Item
- There are no files associated with this item.
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