Neural-Network-Based Adaptive Backstepping Control With Application to Spacecraft Attitude Regulation

被引:106
|
作者
Cao, Xibin [1 ]
Shi, Peng [2 ,3 ]
Li, Zhuoshi [1 ]
Liu, Ming [1 ]
机构
[1] Harbin Inst Technol, Sch Astronaut, Harbin 150001, Heilongjiang, Peoples R China
[2] Univ Adelaide, Sch Elect & Elect Engn, Adelaide, SA 5005, Australia
[3] Victoria Univ, Coll Engn & Sci, Melbourne, Vic 8001, Australia
基金
中国国家自然科学基金; 澳大利亚研究理事会;
关键词
Actuator degradation; adaptive control; backstepping control; neural network; spacecraft attitude regulation; FAULT-TOLERANT CONTROL; OUTPUT-FEEDBACK CONTROL; TIME-DELAY SYSTEMS; STOCHASTIC-SYSTEMS; CONTROL ALLOCATION; ACCOMMODATION; STATE;
D O I
10.1109/TNNLS.2017.2756993
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
This paper investigates the neural-network-based adaptive control problem for a class of continuous-time nonlinear systems with actuator faults and external disturbances. The model uncertainties in the system are not required to satisfy the norm-bounded assumption, and the exact information for components faults and external disturbance is totally unknown, which represents more general cases in practical systems. An indirect adaptive backstepping control strategy is proposed to cope with the stabilization problem, where the unknown nonlinearity is approximated by the adaptive neural-network scheme, and the loss of effectiveness of actuators faults and the norm bounds of exogenous disturbances are estimated via designed online adaptive updating laws. The developed adaptive backstepping control law can ensure the asymptotic stability of the fault closedloop system despite of unknown nonlinear function, actuator faults, and disturbances. Finally, an application example based on spacecraft attitude regulation is provided to demonstrate the effectiveness and the potential of the developed new neural adaptive control approach.
引用
收藏
页码:4303 / 4313
页数:11
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