Retrofit fault-tolerant tracking control design of an unmanned quadrotor helicopter considering actuator dynamics

被引:37
作者
Liu, Zhixiang [1 ]
Yuan, Chi [1 ]
Yu, Xiang [1 ]
Zhang, Youmin [1 ]
机构
[1] Concordia Univ, Dept Mech Ind & Aerosp Engn, 1455 Maisonneuve Blvd W, Montreal, PQ H3G 1M8, Canada
基金
中国国家自然科学基金; 加拿大自然科学与工程研究理事会;
关键词
actuator dynamics; actuator faults; adaptive control; fault estimation; fault-tolerant tracking control (FTTC); linear matrix inequality (LMI); unmanned quadrotor helicopter (UQH); SLIDING MODE CONTROL; FLIGHT CONTROL; UAV; INPUT; FTC; DIAGNOSIS; OBSERVER; VEHICLES; SUBJECT;
D O I
10.1002/rnc.3889
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a retrofit fault-tolerant tracking control (FTTC) design method with application to an unmanned quadrotor helicopter (UQH). The proposed retrofit fault-tolerant tracking controller is developed to accommodate loss-of-effectiveness faults in the actuators of UQH. First, a state feedback tracking controller acting as the normal controller is designed to guarantee the stability and satisfactory performance of UQH in the absence of actuator faults, while actuator dynamics of UQH are also considered in the controller design. Then, a retrofit control mechanism with integration of an adaptive fault estimator and an adaptive fault compensator is devised against the adverse effects of actuator faults. Next, the proposed retrofit FTTC strategy, which is synthesized by the normal controller and an additional reconfigurable fault compensating mechanism, takes over the control of the faulty UQH to asymptotically stabilize the closed-loop system with an acceptable performance degradation in the presence of actuator faults. Finally, both numerical simulations and practical experiments are conducted in order to demonstrate the effectiveness of the proposed FTTC methodology on the asymptotic convergence of tracking error for several combinations of loss-of-effectiveness faults in actuators.
引用
收藏
页码:5293 / 5313
页数:21
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