TY - GEN
T1 - Adaptive attitude coordination control for spacecraft with actuator faults and external disturbances
AU - Huang, Yuqing
AU - Wang, Chenliang
AU - Jia, Jindou
AU - Xing, Lantao
N1 - Publisher Copyright:
© 2020 IEEE.
PY - 2020/11/6
Y1 - 2020/11/6
N2 - In this paper, a spacecraft attitude adaptive coordination control scheme is proposed, which considered the external disturbances and actuator faults that are time varying and unknown. By this control method, the time-varying multiplicative and additive actuator faults are solved, and the external disturbances was compensated. The attitude tracking error by the boundary function and the error conversion function can converge to a given range. Finally, the control scheme is demonstrated to be effective by the simulation results.
AB - In this paper, a spacecraft attitude adaptive coordination control scheme is proposed, which considered the external disturbances and actuator faults that are time varying and unknown. By this control method, the time-varying multiplicative and additive actuator faults are solved, and the external disturbances was compensated. The attitude tracking error by the boundary function and the error conversion function can converge to a given range. Finally, the control scheme is demonstrated to be effective by the simulation results.
KW - Adaptive control
KW - actuator faults
KW - coordination control
KW - spacecraft
KW - specified performance
UR - https://www.scopus.com/pages/publications/85100916100
U2 - 10.1109/CAC51589.2020.9326757
DO - 10.1109/CAC51589.2020.9326757
M3 - 会议稿件
AN - SCOPUS:85100916100
T3 - Proceedings - 2020 Chinese Automation Congress, CAC 2020
SP - 1494
EP - 1499
BT - Proceedings - 2020 Chinese Automation Congress, CAC 2020
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2020 Chinese Automation Congress, CAC 2020
Y2 - 6 November 2020 through 8 November 2020
ER -