Observer-based backstepping longitudinal control for carrier-based UAV with actuator faults

被引:36
作者
Zheng, Fengying [1 ]
Zhen, Ziyang [2 ]
Gong, Huajun [2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, Nanjing 210016, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China
基金
高等学校博士学科点专项科研基金;
关键词
constraint backstepping; fuzzy observer; carrier-based UAV; flight control system; fault tolerant; FLIGHT CONTROL; TOLERANT CONTROL; NEURAL-NETWORKS; CONTROL-SYSTEM; DESIGN; APPROXIMATION; TRACKING; VEHICLE;
D O I
10.21629/JSEE.2017.02.14
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The paper presents the longitudinal control for the carrier-based unmanned aerial vehicle (UAV) system with unmeasured states, actuator faults, control input constraints, and external disturbances. By combining output state observer, adaptive fuzzy control, and constraint backstepping technology, a robust fault tolerant control approach is proposed. An output state observer with fuzzy logic systems is developed to estimate unmeasured states, and command filters rather than differentiations of virtual control law are used to solve the computational complexity problem in traditional backstepping. Additionally, a robust term is introduced to offset the fuzzy adaptive estimation error and external disturbance, and an appropriate fault controller structure with matching conditions obtained from fault compensation is proposed. Based on the Lyapunov theory, the designed control program is illustrated to guarantee that all the closed-loop signals of the given system are bounded, and the output errors converge to a small neighborhood of zero. A carrier-based UAV nonlinear longitudinal model is employed to testify the feasibility and validity of the control scheme. The simulation results show that all the controllers can perform at a satisfactory level of reference tracking despite the existence of unknown aerodynamic parameters and actuator faults.
引用
收藏
页码:322 / 337
页数:16
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