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학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
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논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 발행연도
- 2009.8
- 수록면
- 5,194 - 5,198 (5page)
이용수
초록· 키워드
오류제보하기
We consideratar get pointing problem of a space craft which has fewer control torques than the degrees of freedom to be controlled. In addition, we consider the failures of attitude sensors. To over come such failure situations, a novel method to represent control error, with out applying any complicated attitude estimation algorithm, is proposed using geomagnetic field measurements. The proposed error representation does not require any toqueon an axis which loses control. We derive a feedback control law that globally and a symptoticallys tabilizes the space craft about the underactuated space craftax is along the speciied target direction in a ninertial frame. Simulation was carried out and results are presented illustrating the efficacy of the proposed algorithm under the condition of measurement uncertanties and environmental disturbances.
목차
Abstract
1.INTRODUCTION
2.MAIL RESULTS
3.NUMERICAL SIMULATION
4.CONCLUDING REMARK
REFERENCES
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UCI(KEPA) : I410-ECN-0101-2014-569-000762019