Adaptive fault tolerant control for trajectory tracking of a quadrotor helicopter

被引:20
作者
Li, Min [1 ,4 ]
Zuo, Zongyu [1 ]
Liu, Hao [2 ]
Liu, Cunjia [3 ]
Zhu, Bing [1 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Astronaut, Beijing, Peoples R China
[3] Loughborough Univ, Dept Aeronaut & Automot Engn, Loughborough, Leics, England
[4] Shanghai Radio Equipment Res Inst, Shanghai, Peoples R China
基金
中国国家自然科学基金;
关键词
Quadrotor; trajectory tracking; fault tolerant control; adaptive control; low-pass filters; GUARANTEED ROBUSTNESS; SYSTEMS;
D O I
10.1177/0142331217728568
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, an adaptive fault tolerant controller based on L-1 control is developed and applied to the trajectory tracking for a quadrotor helicopter. Both multiplicative and additive actuator faults are considered. The proposed design is based on nonlinear feed-forward compensations and a typical nonlinear quadrotor model with uncertain inertial parameters and external disturbances. The L-1 adaptive control design is slightly modified to adapt with the position and the attitude error dynamics. The proposed adaptive controller yields uniformly verifiable bounds on the transient and the steady-state tracking error for any designated bounded reference trajectory. In the presence of fast adaptation, the adaptive controller compensates for actuator fault and disturbances in a particular frequency range. Finally, simulation results are included to validate the effectiveness of the proposed design.
引用
收藏
页码:3560 / 3569
页数:10
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