TY - GEN
T1 - Application of sliding mode control based on disturbance observer on high performance flight motion simulator
AU - Wu, Yunjie
AU - Le, Weiting
AU - Tian, Dapeng
PY - 2007
Y1 - 2007
N2 - For flight motion simulator servo system, this paper presents a kind of robust discrete sliding mode controller based on disturbance observer. The entire system is composed of two parts: one is the design of disturbance observer and the other is the design of discrete sliding mode controller. Sliding mode controller (SMC) is a special nonlinear control strategy, which has strong robustness against parameter variations, load disturbances and uncertainty of system, but the chattering produced by sliding mode control limits Its application to the practical system. In this paper, by using disturbance observer technology, the external disturbances can be compensated and the SMC control law can be used successfully, and the chattering can be effectively alleviated. The proposed controller is adopted in flight motion simulator servo system. Simulation and real system experiment results confirm the effectiveness of the proposed control method.
AB - For flight motion simulator servo system, this paper presents a kind of robust discrete sliding mode controller based on disturbance observer. The entire system is composed of two parts: one is the design of disturbance observer and the other is the design of discrete sliding mode controller. Sliding mode controller (SMC) is a special nonlinear control strategy, which has strong robustness against parameter variations, load disturbances and uncertainty of system, but the chattering produced by sliding mode control limits Its application to the practical system. In this paper, by using disturbance observer technology, the external disturbances can be compensated and the SMC control law can be used successfully, and the chattering can be effectively alleviated. The proposed controller is adopted in flight motion simulator servo system. Simulation and real system experiment results confirm the effectiveness of the proposed control method.
KW - Disturbance observer
KW - Flight simulator
KW - Servo system
KW - Sliding mode
UR - https://www.scopus.com/pages/publications/40649090187
U2 - 10.1109/ICAL.2007.4339037
DO - 10.1109/ICAL.2007.4339037
M3 - 会议稿件
AN - SCOPUS:40649090187
SN - 1424415314
SN - 9781424415311
T3 - Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2007
SP - 2695
EP - 2699
BT - Proceedings of the IEEE International Conference on Automation and Logistics, ICAL 2007
T2 - 2007 IEEE International Conference on Automation and Logistics, ICAL 2007
Y2 - 18 August 2007 through 21 August 2007
ER -