Signal corrector and decoupling estimations for UAV control

被引:2
|
作者
Wang, X. [1 ]
机构
[1] Univ Nottingham, Aerosp Engn, Nottingham, England
来源
AERONAUTICAL JOURNAL | 2023年 / 127卷 / 1311期
关键词
Large-error sensing; Uncertainty; Signal corrector; Decoupling estimation; ATTITUDE;
D O I
10.1017/aer.2022.86
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
For a class of uncertain systems with large-error sensing, the low-order stable signal corrector and observer are presented for signal correction and uncertainty estimation according to completely decoupling estimation. The model-free signal corrector can reject the bounded stochastic disturbance/error in global position sensing, and system uncertainty can be estimated by the observer, even the existence of large disturbance in position sensing. Furthermore, a general form of signal corrector is given. The describing function method is used to analyse the robustness of the corrector in frequency domain, and the parameter selection rules are presented. The merits of the signal corrector includes its model free, gain-bounded stable structure, sufficient rejection of bounded stochastic disturbance/error in sensing and ease of parameters' regulation. The corrector and observer are applied to a UAV navigation and control for large disturbance/error corrections in position/attitude angle and the uncertainties estimation in the UAV flight dynamics. The control laws are designed according to the correction-estimation results. Finally, experiments demonstrate the effectiveness of the proposed method.
引用
收藏
页码:796 / 817
页数:22
相关论文
共 50 条
  • [1] Sliding mode corrector for jet UAV control
    Wang, X.
    AERONAUTICAL JOURNAL, 2023, 128 (1319): : 37 - 72
  • [2] Nonlinear predictive decoupling control of Rotorcraft UAV using serial decoupling method
    Ruan, Xiaogang
    Hou, Xuyang
    INDUSTRIAL INSTRUMENTATION AND CONTROL SYSTEMS, PTS 1-4, 2013, 241-244 : 1240 - 1247
  • [3] The Attitude Decoupling Control Of The Flying Wing UAV (IEEE CGNCC)
    Li, Jiguang
    Chen, Xin
    Li, Zhen
    2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 357 - 362
  • [4] Parallel Compensation Control of Power Factor Corrector Without Electrolytic Capacitor by Power Decoupling
    Wang L.
    Cui S.
    Chen M.
    Diangong Jishu Xuebao/Transactions of China Electrotechnical Society, 2019, 34 (03): : 516 - 528
  • [5] A decoupling control for quadrotor UAV using dynamic surface control and sliding mode disturbance observer
    Lin, Xiaobo
    Yu, Yao
    Sun, Chang-yin
    NONLINEAR DYNAMICS, 2019, 97 (01) : 781 - 795
  • [6] A decoupling control for quadrotor UAV using dynamic surface control and sliding mode disturbance observer
    Xiaobo Lin
    Yao Yu
    Chang-yin Sun
    Nonlinear Dynamics, 2019, 97 : 781 - 795
  • [7] Combating the Control Signal Spoofing Attack in UAV Systems
    Huang, Ke-Wen
    Wang, Hui-Ming
    IEEE TRANSACTIONS ON VEHICULAR TECHNOLOGY, 2018, 67 (08) : 7769 - 7773
  • [8] Design of a Fully Actuated Passively Tilted Multirotor UAV with Decoupling Control System
    Kotarski, Denis
    Piljek, Petar
    Brezak, Hrvoje
    Kasac, Josip
    2017 8TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE), 2017, : 385 - 390
  • [9] A New Series Compensation Control Strategy of Power Factor Corrector Without Electrolytic Capacitor by Power Decoupling
    Wang L.
    Wang H.
    Cui S.
    Shen H.
    Zhongguo Dianji Gongcheng Xuebao/Proceedings of the Chinese Society of Electrical Engineering, 2019, 39 (17): : 5195 - 5204
  • [10] A New Parallel Compensation Control Strategy of Power Factor Corrector without Electrolytic Capacitor by Power Decoupling
    Wang, Liqiao
    Wang, Haixu
    Cui, Shumin
    Chen, Mei
    Shen, Hong
    2018 IEEE INTERNATIONAL POWER ELECTRONICS AND APPLICATION CONFERENCE AND EXPOSITION (PEAC), 2018, : 69 - 74