TY - GEN
T1 - Fault-Tolerant control for flexible spacecraft attitude maneuver via integral sliding mode control approach
AU - Fu, Jingbo
AU - Liu, Ming
AU - Chen, Lei
N1 - Publisher Copyright:
© 2015 IEEE.
PY - 2016/1/13
Y1 - 2016/1/13
N2 - An integral sliding mode fault-Tolerant control scheme is developed to investigate the problem of flexible spacecraft attitude maneuver. The designed approach is robust and insensitive to external perturbations and model uncertainty resulted from measuring error of the inertia matrix and partial loss of actuator effectiveness. The use of proportional-integral controller reduce the chattering phenomena in sliding mode control scheme. Hence, we can achieve a more appropriate control accuracy. Finally, simulation results are included to demonstrate the effectiveness of this method.
AB - An integral sliding mode fault-Tolerant control scheme is developed to investigate the problem of flexible spacecraft attitude maneuver. The designed approach is robust and insensitive to external perturbations and model uncertainty resulted from measuring error of the inertia matrix and partial loss of actuator effectiveness. The use of proportional-integral controller reduce the chattering phenomena in sliding mode control scheme. Hence, we can achieve a more appropriate control accuracy. Finally, simulation results are included to demonstrate the effectiveness of this method.
KW - attitude stabilization
KW - flexible spacecraft
KW - integral sliding mode
KW - second-order sliding mode
UR - https://www.scopus.com/pages/publications/84966526002
U2 - 10.1109/CAC.2015.7382786
DO - 10.1109/CAC.2015.7382786
M3 - 会议稿件
AN - SCOPUS:84966526002
T3 - Proceedings - 2015 Chinese Automation Congress, CAC 2015
SP - 1750
EP - 1754
BT - Proceedings - 2015 Chinese Automation Congress, CAC 2015
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - Chinese Automation Congress, CAC 2015
Y2 - 27 November 2015 through 29 November 2015
ER -