Adaptive quantized fault-tolerant control of a 2-DOF helicopter system with actuator fault and unknown dead zone

被引:27
|
作者
Zhao, Zhijia [1 ]
Zhang, Jian [1 ]
Liu, Zhijie [2 ,3 ]
He, Wei [2 ,3 ]
Hong, Keum-Shik [4 ]
机构
[1] Guangzhou Univ, Sch Mech & Elect Engn, Guangzhou 510006, Peoples R China
[2] Univ Sci & Technol Beijing, Sch Intelligence Sci & Technol, Beijing 100083, Peoples R China
[3] Univ Sci & Technol Beijing, Inst Artificial Intelligence, Beijing 100083, Peoples R China
[4] Pusan Natl Univ, Sch Mech Engn, 2 Busandaehak Ro, Busan 46241, South Korea
基金
中国国家自然科学基金;
关键词
Adaptive control; Quantized control; Fault -tolerant control; 2-DOF helicopter; Unknown dead zone; ATTITUDE TRACKING CONTROL; NONLINEAR-SYSTEMS; NEURAL-NETWORK; INPUT;
D O I
10.1016/j.automatica.2022.110792
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 study proposes an adaptive quantized fault-tolerant control for a nonlinear two-degree of freedom (2-DOF) helicopter system with an unknown dead zone and actuator failures. First, a hysteresis quantizer is employed to reduce the jittering during signal quantization. Second, a radial basis function neural network is adopted to address the uncertainty in the nonlinear helicopter system. Bounded estimates, smoothing functions, and adaptive parameters are used to compensate for the effects of unknown dead zones, actuator faults, and quantization inputs. Subsequently, an adaptive neural network quantized fault-tolerant control strategy is developed for the nonlinear 2-DOF helicopter system using a backstepping technique. In addition, the closed-loop system is proved to be semi -globally uniformly bounded using rigorous Lyapunov stability analysis. Finally, the effectiveness of the derived control strategy is demonstrated through simulation and experimental results.(c) 2022 Elsevier Ltd. All rights reserved.
引用
收藏
页数:10
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