Fixed-time three-dimensional guidance law with input constraint and actuator faults

被引:4
作者
Li, Peng [1 ]
Liu, Qi [1 ]
He, Chen-Yu [1 ]
Liu, Xiao-Qing [2 ]
机构
[1] Xiangtan Univ, Sch Automat & Elect Informat, Xiangtan, Peoples R China
[2] Tsinghua Univ, Dept Precis Instrument, Beijing 100084, Peoples R China
关键词
Three-dimensional guidance; nonhomogeneous disturbance observer; fault-tolerant control; input constraint; TERMINAL SLIDING MODE; TRACKING CONTROL; PROPORTIONAL NAVIGATION; HYPERSONIC VEHICLE; MISSILE;
D O I
10.1177/0954410020971973
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper investigates the three-dimensional guidance with the impact angle constraint, actuator faults and input constraint. Firstly, an adaptive three-dimensional guidance law with impact angle constraint is designed by using the terminal sliding mode control and nonhomogeneous disturbance observer. Then, in order to solve the problem of the input saturation and actuator faults, an adaptive anti-saturation fault-tolerant three-dimensional law is proposed by using the hyperbolic tangent function based on the passive fault-tolerant control. Finally, the effectiveness of the designed guidance laws is verified by using the Lyapunov function and simulation.
引用
收藏
页码:1274 / 1283
页数:10
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