Q-learning-based practical disturbance compensation control for hypersonic flight vehicle

被引:2
|
作者
Li, Xu [1 ,2 ]
Zhang, Ziyi [1 ,2 ]
Ji, Yuehui [1 ,2 ]
Liu, Junjie [1 ,2 ]
Gao, Qiang [1 ,2 ]
机构
[1] Tianjin Univ Technol, Sch Elect Engn & Automation, Bldg 29,391 Binshuixi Rd, Tianjin, Peoples R China
[2] Tianjin Key Lab Control Theory & Applicat Complica, Tianjin, Peoples R China
基金
中国国家自然科学基金;
关键词
Hypersonic flight vehicle; attitude control; super-twisting algorithm; extended state observer; Q-learning; FAULT-TOLERANT CONTROL; SLIDING MODE CONTROL; REJECTION CONTROL; ADAPTIVE-CONTROL; ATTITUDE-CONTROL; CONTROL SCHEME; DESIGN; STRATEGY; GAME; GO;
D O I
10.1177/09544100221140242
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Aiming at the attitude control problem of hypersonic flight vehicle, a compound control strategy based on the disturbance compensation technique and Q-learning optimization is proposed. Firstly, a three-channel independent control scheme based on the super-twisting extended state observer (STESO) is proposed such that coupling among channels, uncertainties, and external disturbances can be estimated and compensated in real time. Secondly, the Q-learning mechanism is introduced to optimize the control parameters while keeping the control structure unchanged. Lastly, the convergence of the STESO is analyzed by the Lyapunov theory, and some numerical simulation results are carried out to verify the effectiveness of the proposed strategy. Compared with the traditional linear active disturbance rejection control, the proposed method can avoid a lot of manual parameter tuning process and also has better performance.
引用
收藏
页码:1916 / 1929
页数:14
相关论文
共 50 条
  • [21] Longitudinal inversion flight control based on backstepping for hypersonic vehicle
    College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    Kongzhi yu Juece Control Decis, 2007, 3 (313-317):
  • [22] Neural Network Modeling-Based Anti-Disturbance Tracking Control for Hypersonic Flight Vehicle Models
    Xu Lubing
    Yi Yang
    Shao Liren
    Zheng Weixing
    PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 1311 - 1316
  • [23] Q-Learning-based parameters adaptive algorithm for active disturbance rejection control and its application to ship course control
    Chen, Zengqiang
    Qin, Beibei
    Sun, Mingwei
    Sun, Qinglin
    NEUROCOMPUTING, 2020, 408 : 51 - 63
  • [24] Reinforcement Learning based Optimal Tracking Control for Hypersonic Flight Vehicle: A Model Free Approach
    Hu, Xiaoxiang
    Dong, Kejun
    Yang, Teng
    Xiao, Bing
    2022 IEEE 20TH INTERNATIONAL CONFERENCE ON INDUSTRIAL INFORMATICS (INDIN), 2022, : 711 - 717
  • [25] Q-learning-based routing inspired by adaptive flocking control for collaborative unmanned aerial vehicle swarms
    Alam, Muhammad Morshed
    Moh, Sangman
    VEHICULAR COMMUNICATIONS, 2023, 40
  • [26] Adaptive diagnosis and compensation for hypersonic flight vehicle with multisensor faults
    Chen, Fuyang
    Gong, Jingxiu
    Li, Yuqing
    INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2019, 29 (17) : 6145 - 6163
  • [27] Iterative Q-Learning-Based Nonlinear Optimal Tracking Control
    Wei, Qinglai
    Song, Ruizhuo
    Xu, Yancai
    Liu, Derong
    PROCEEDINGS OF 2016 IEEE SYMPOSIUM SERIES ON COMPUTATIONAL INTELLIGENCE (SSCI), 2016,
  • [28] Recursive terminal sliding mode control for hypersonic flight vehicle with sliding mode disturbance observer
    Jianmin Wang
    Yunjie Wu
    Xiaomeng Dong
    Nonlinear Dynamics, 2015, 81 : 1489 - 1510
  • [29] Switching Control Design for A Hypersonic Flight Vehicle
    Tan, Shuping
    Li, Zhibin
    2010 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-5, 2010, : 3568 - 3573
  • [30] Dynamic Characteristic and Control of a Hypersonic Flight Vehicle
    Qin, Dongsheng
    Zhu, Qiangjun
    Wang, Chenxi
    PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON COMPUTER, NETWORKS AND COMMUNICATION ENGINEERING (ICCNCE 2013), 2013, 30 : 29 - 33