Quaternion-based adaptive control of a spacecraft with reaction wheels

Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University

Volumn 37, Issue 12, 2003, Pages 1957-1960

  Liu, Yan Zhu ^a   Ma, Xiao Min ^a  

^a SHANGHAI JIAO TONG UNIVERSITY   (China)

Author keywords

Adaptive control; Attitude control; Quaternion

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; ASYMPTOTIC STABILITY; COMPUTER SIMULATION; DYNAMICS; WHEELS;

ATTITUDE CONTROL; EULER ANGLES; LYAPUNOV DIRECT METHOD; QUATERNION BASED ADAPTIVE CONTROL; REACTION WHEELS;

SPACECRAFT;

EID: 2442655516     PISSN: 10062467     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (9)

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3. CHEN Wan-chun, XIAO Ye-lun, ZHAO Li-hong, et al. Quaternion and its application in attitude control of spacecraft [J]. Journal of Aeronautics, 2000, 21(5): 389-392.
4. FENG Lu, GONG Cheng, HE Chang-an. A sliding-mode controller of attitude tracking system of vehicle based on error-quaternion [J]. Journal of Astronautics, 2000, 21(1): 17-22.
5. LIU Yan-zhu. Calculation of the error of quaternion [J]. Mechanics in Engineering, 2003, 25(2): 70-71.
6. Slotine J-J E, Di Benedetto M D. Hamiltonian adaptive control of spacecraft [J]. IEEE Transactions on Automatic Control, 1990, 35(7): 848-852.