Adaptive model-free fault-tolerant control based on integral reinforcement learning for a highly flexible aircraft with actuator faults

被引:17
作者
Ma, Jianjun [1 ]
Peng, Chi [1 ]
机构
[1] Natl Univ Def Technol, Coll Intelligence Sci & Technol, Changsha 410073, Hunan, Peoples R China
关键词
Model-free; Fault-tolerant control; Integral reinforcement learning; Highly flexible aircraft; Observer-like reference model; OPTIMAL TRACKING CONTROL; TIME LINEAR-SYSTEMS; NONLINEAR-SYSTEMS; FAILURE COMPENSATION; ROBUST; DESIGN;
D O I
10.1016/j.ast.2021.107204
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article presents an adaptive model-free fault-tolerant control scheme based on integral reinforcement learning (IRL) technique for tracking control of a highly flexible aircraft (HFA) with actuator faults. To begin, the integral of the tracking error is introduced as a new state to construct an augmented system for the control design. Following that, the off-policy IRL method is applied to obtain the optimal feedback control law online in order to solve the tracking problem without system knowledge. Furthermore, in order to effectively handle system uncertainties, external disturbances, and actuator faults, an adaptive model-free fault-tolerant controller with an observer-like reference model is developed. The designed controller can guarantee that the closed-loop system is uniformly bounded and the tracking error asymptotically approaches zero by choosing design parameters appropriately. Finally, numerical simulations demonstrate the desirable fault accommodation capability of the proposed fault-tolerant strategy. (c) 2021 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:14
相关论文
共 49 条
[1]  
[Anonymous], 1991, APPL NONLINEAR CONTR
[2]   KRONECKER PRODUCTS AND MATRIX CALCULUS IN SYSTEM THEORY [J].
BREWER, JW .
IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS, 1978, 25 (09) :772-781
[3]   Sliding-Mode Control Strategies for Rendezvous and Docking Maneuvers [J].
Capello, Elisa ;
Punta, Elisabetta ;
Dabbene, Fabrizio ;
Guglieri, Giorgio ;
Tempo, Roberto .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (06) :1481-+
[4]   Sensor-Fault Detection, Isolation and Accommodation for Digital Twins via Modular Data-Driven Architecture [J].
Darvishi, Hossein ;
Ciuonzo, Domenico ;
Eide, Eivind Roson ;
Rossi, Pierluigi Salvo .
IEEE SENSORS JOURNAL, 2021, 21 (04) :4827-4838
[5]  
Gibson T., 2011, AIAA GUIDANCE NAVIGA, P6202
[6]   Adaptive Output Feedback Based on Closed-Loop Reference Models [J].
Gibson, Travis E. ;
Qu, Zheng ;
Annaswamy, Anuradha M. ;
Lavretsky, Eugene .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2015, 60 (10) :2728-2733
[7]   A novel active fault-tolerant control for spacecrafts with full state constraints and input saturation [J].
Hu, Hui ;
Wang, Bo ;
Cheng, Zhongtao ;
Liu, Lei ;
Wang, Yongji ;
Luo, Xiaoli .
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 108
[8]   Delta Operator-Based Fault Estimation and Fault-Tolerant Model Predictive Control for Steer-By-Wire Systems [J].
Huang, Chao ;
Naghdy, Fazel ;
Du, Haiping .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2018, 26 (05) :1810-1817
[9]   Fault-tolerant control systems: A comparative study between active and passive approaches [J].
Jiang, Jin ;
Yu, Xiang .
ANNUAL REVIEWS IN CONTROL, 2012, 36 (01) :60-72
[10]   Computational adaptive optimal control for continuous-time linear systems with completely unknown dynamics [J].
Jiang, Yu ;
Jiang, Zhong-Ping .
AUTOMATICA, 2012, 48 (10) :2699-2704