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http://dx.doi.org/10.5139/JKSAS.2010.38.1.042

Fault Tolerant Attitude Control of a Spacecraft Using Two Wheels  

Jin, Jae-Hyun (순천대학교 우주항공공학)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.38, no.1, 2010 , pp. 42-47 More about this Journal
Abstract
This paper considers a fault tolerant control problem for a spacecraft using wheels which are momentum exchanging devices. The control of a satellite with only two healthy wheels has been studied and its result has been presented. Two different configurations have been considered. When the yaw rate cannot be controlled directly by any control input, the desired yaw rate can be obtained by using the roll rate as a pseudo control. As a result, all three angular speeds have been stabilized, and two attitude angles including pitch and yaw have been controlled to converge to the desired values.
Keywords
Spacecraft attitude control; Fault tolerant control; Reaction wheel; Underactuation;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
1 Kim, S., and Kim, Y., “Spin axis stabilization of a rigid spacecraft using two reaction wheels”, Journal of Guidance, Control, and Dynamics, Vol.24, No.5, 2001, pp. 1046-1049.   DOI   ScienceOn
2 이승우, 고현철, 장우영, 손준원, “피치 모멘텀 바이어스 위성시스템의 롤/요축 모멘텀 제어방식”, 한국항공우주학회지, 제37권 제7호, 2009, pp. 669-677.   과학기술학회마을   DOI   ScienceOn
3 Bang, H., Tahk, M., and Choi, H., "Large angle attitude control of spacecraft with actuator saturation", Control Engineering Practice, Vol. 11, No. 9, 2003, pp. 989-997.   DOI   ScienceOn
4 진재현, 이훈구, 탁민제, “반작용 휠을 사용하는 인공위성의 내고장 자세제어기법”, 한국항공우주학회지, 제35권 제6호, 2007, pp. 526-532.   과학기술학회마을   DOI   ScienceOn
5 Crouch, P., “Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models”, IEEE Transaction on Automatic Control, Vol. 29, No. 4, 1984, pp. 321-331.   DOI
6 Marshall, A., and Tsiotras, P., “Spacecraft angular velocity stabilization using a single gimbal variable speed control moment gyro”, AIAA Paper 03-5654, 2003.
7 Krishnan, H., McClamroch, N., and Reyhanoglu, M., “Attitude stabilization of a rigid spacecraft using two momentum wheel actuators”, Journal of Guidance, Control, and Dynamics, Vol.18, No.2, 1995, pp. 256-263.   DOI   ScienceOn
8 김성필, 김유단, “두개의 모멘텀휠을 이용한 강체위성의 자세안정화기법”, 한국항공우주학회지, 제29권 제4호, 2001, pp.78-85.
9 황재혁 , 이성춘 , 오화석 , 은종원, “불완전 리액션 휠 세트를 갖는 위성의 자세 제어기법 연구”, 한국항공우주학회지, 제25권 제4호, 1997, pp. 114-122.
10 Tsiotras, P., and Longuski, J., “Spin-axis stabilization of symmetric spacecraft with two control torques”, Systems and Control Letters, Vol. 23, No. 6, 1994, pp. 395-402.   DOI   ScienceOn