Active Fault-Tolerant Control for Quadrotor UAV against Sensor Fault Diagnosed by the Auto Sequential Random Forest

被引:14
作者
Ai, Shaojie [1 ,2 ]
Song, Jia [1 ,2 ]
Cai, Guobiao [1 ,3 ]
Zhao, Kai [1 ,2 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Beihang Univ, Aerosp Crafts Technol Inst, Beijing 100191, Peoples R China
[3] Beihang Univ, Minist Educ, Key Lab Spacecraft Design Optimizat & Dynam Simul, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
active fault-tolerant control; active disturbance rejection control; quadrotor unmanned aerial vehicle; sensor fault; fault diagnosis; random forest; TRACKING CONTROL; SYSTEM; AIRCRAFT; FILTER;
D O I
10.3390/aerospace9090518
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Active disturbance rejection control (ADRC) is a model-independent method widely used in passive fault-tolerant control of the quadrotor unmanned aerial vehicle. While ADRC's effectiveness in actuator fault treatment has been proven, its tolerance to sensor faults requires improvements. In this paper, an ADRC-based active fault-tolerant control (AFTC) scheme is proposed to control the flying attitude against sensor fault for reliability enhancement. Specifically, a semi-model-dependent state tracker is raised to reduce the influence of slow tracking, and accentuate the sensor fault even in varying maneuvers. Derived from the random forest, an enhanced method named auto sequential random forest is designed and applied to isolate and identify faults in real time. Once the tolerance compensation is generated with the fault information, a high-performance AFTC is achieved. The simulation results show that the proposed method can effectively follow the residual when a sensor fault and a change of maneuver occur concurrently. Precise fault information is obtained within 0.04 s, even for small faults on the noise level. The diagnosis accuracy is greater than 86.05% (100% when small faults are excluded), and the identification precision exceeds 97.25%. The short settling time (0.176 s when the small fault is excluded) and modest steady-state error validate the advanced and robust tolerance performance of the proposed AFTC method.
引用
收藏
页数:25
相关论文
共 38 条
[31]   Fully distributed time-varying formation tracking control for multiple quadrotor vehicles via finite-time convergent extended state observer [J].
Zhang, Wenqiang ;
Dong, Chaoyang ;
Ran, Maopeng ;
Liu, Yang .
CHINESE JOURNAL OF AERONAUTICS, 2020, 33 (11) :2907-2920
[32]   Deep Deterministic Policy Gradient-Based Active Disturbance Rejection Controller for Quad-Rotor UAVs [J].
Zhao, Kai ;
Song, Jia ;
Hu, Yunlong ;
Xu, Xiaowei ;
Liu, Yang .
MATHEMATICS, 2022, 10 (15)
[33]   High-order sliding mode observer-based trajectory tracking control for a quadrotor UAV with uncertain dynamics [J].
Zhao, Zhenhua ;
Cao, Dong ;
Yang, Jun ;
Wang, Huiming .
NONLINEAR DYNAMICS, 2020, 102 (04) :2583-2596
[34]   Active fault-tolerant tracking control of a quadrotor with model uncertainties and actuator faults [J].
Zhong, Yu-jiang ;
Liu, Zhi-xiang ;
Zhang, You-min ;
Zhang, Wei ;
Zuo, Jun-yi .
FRONTIERS OF INFORMATION TECHNOLOGY & ELECTRONIC ENGINEERING, 2019, 20 (01) :95-106
[35]  
Zhou LS, 2017, CHIN CONTR CONF, P7321, DOI 10.23919/ChiCC.2017.8028513
[36]   Online condition diagnosis for a two-stage gearbox machinery of an aerospace utilization system using an ensemble multi-fault features indexing approach [J].
Zhou, Min ;
Wang, Ke ;
Wang, Yang ;
Luo, Kaijia ;
Fu, Hongyong ;
Si, Liang .
CHINESE JOURNAL OF AERONAUTICS, 2019, 32 (05) :1100-1110
[37]   Sensors Fault Diagnosis and Active Fault-Tolerant Control for PMSM Drive Systems Based on a Composite Sliding Mode Observer [J].
Zhu, Qinyue ;
Li, Zhaoyang ;
Tan, Xitang ;
Xie, Dabo ;
Dai, Wei .
ENERGIES, 2019, 12 (09)
[38]   Robust Fault-Tolerant Control for Underactuated Takeoff and Landing UAVs [J].
Zou, Yao ;
Xia, Kewei .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2020, 56 (05) :3545-3555