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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences KSAS International Journal Volume.5 Number.1
- 발행연도
- 2004.5
- 수록면
- 19 - 29 (11page)
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초록· 키워드
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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 boundary constraints. Sensitivity of the switching times with respect to modal parameters could be a critical factor degrading the performance of the time optimal solutions. A new approach for the robustness enhancement of switching times with respect to modal parameter uncertainty is introduced. A new concept so-called augmented dynamic model is added to account for the modal uncertainty. The proposed approach turns out to be similar to some previous methods, but it essentially provides some new results.
목차
Abstract
Introduction
Time Optimal Control
Robust Time-Optimal Control
Simulation Results
Concluding Remarks
Aknowledgement
References
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