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학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 발행연도
- 2004.1
- 수록면
- 122 - 131 (10page)
이용수
초록· 키워드
오류제보하기
A constraint equation-based control law design for large angle attitude maneuvers of flexible spacecraft is addressed in this paper. The tip displacement of the flexible spacecraft model is prescribed in the form of a constraint equation. The controller design is attempted in the way that the constraint equation is satisfied throughout the maneuver. The constraint equation leads to a two-point boundary value problem which needs backward and forward solution techniques to satisfy terminal constraints. An observer-based tracking control law takes the constraint equation as the input to the dynamic observer. The observer state is used in conjunction with the state feedback control law to have the actual system follow the observer dynamics. The observer-based tracking control law eventually turns into a stabilized system with inherent nature of robustness and disturbance rejection in LQR type control laws.
목차
Abstract
1.Introduction
2.Dynamics and Modeling
3.Control Law Design
4.Simulation and Analysis
5.Conclusions
Acknowledgment
References
참고문헌 (14)
참고문헌 신청
[학술지(정기간행물)] - / 1981 / Optimal Feedback Control for Flexible Spacecraft Journal of Guidance 4 : 427 ~ 479
[학술지(정기간행물)] - / 1983 / Design of Space Structure Control Systems Using On-Off Thrusters Journal of Guidance 6 : 759 ~ 775
[학술지(정기간행물)] - / 1987 / Maneuvering and Vibration Control of Flexible Spacecraft Journal of Astronautical Sciences 35 : 301 ~ 328
[학술지(정기간행물)] - / 1989 / Planar Time Optimal Slewing Maneuvers of Flexible Spacecraft Journal of Guidance 12 : 71 ~ 81
[학술지(정기간행물)] - / / Feedback Control of Flexible Spacecraft Large Angle Maneuvers Using the Liapunov Theory Proceedings of the 1984 American Control Conference Inst. of Electrical and Electronics Engineers : 1674 ~ 1678
[학술지(정기간행물)] - / 1983 / Design of Space Structure Control Systems Using On-Off Thrusters Journal of Guidance 6 : 759 ~ 775
[학술지(정기간행물)] - / 1987 / Maneuvering and Vibration Control of Flexible Spacecraft Journal of Astronautical Sciences 35 : 301 ~ 328
[학술지(정기간행물)] - / 1989 / Planar Time Optimal Slewing Maneuvers of Flexible Spacecraft Journal of Guidance 12 : 71 ~ 81
[학술지(정기간행물)] - / / Feedback Control of Flexible Spacecraft Large Angle Maneuvers Using the Liapunov Theory Proceedings of the 1984 American Control Conference Inst. of Electrical and Electronics Engineers : 1674 ~ 1678
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