UDE-based adaptive dynamic surface control for attitude-constrained reusable launch vehicle

被引:0
|
作者
Mo, Ran [1 ]
Li, Wenting [2 ,3 ]
Su, Shanwei [2 ]
机构
[1] China Special Vehicle Res Inst, Syst Avion Res Off, Jingmen 448035, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[3] Beijing Aerosp Automat Control Inst, Beijing 100070, Peoples R China
关键词
VTLV; Attitude tracking control; Adaptive dynamic surface control; UDE; Attitude constraint; 93-XX; 93Dxx; NEURAL-NETWORK CONTROL; PRESCRIBED PERFORMANCE; NONLINEAR-SYSTEMS; TRACKING CONTROL; INPUT;
D O I
10.1007/s11071-023-09233-9
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents an adaptive dynamic surface control scheme for vertical takeoff and landing reusable launch vehicles (VTLVs) with unknown disturbances, model uncertainties, and an attitude constraint to achieve exact attitude tracking control in the aerodynamic descent phase. First, the six-degree-of-freedom dynamic model of the VTLV is established. Next, the unknown disturbances and model uncertainties in the VTLV model are considered as the total disturbances, which are estimated by employing an uncertainty and disturbance estimator to compensate the controller, thereby enhancing the control accuracy of the system. Moreover, a symmetric time-varying barrier Lyapunov function is utilized to cope with the attitude-constrained problem. Finally, the high tracking performance of the proposed adaptive dynamic surface controller is verified by numerical simulation results.
引用
收藏
页码:5365 / 5378
页数:14
相关论文
共 50 条
  • [31] Reusable launch vehicle attitude control using a time-varying sliding mode control technique
    Shtessel, YB
    Zhu, JJ
    Daniels, D
    PROCEEDINGS OF THE THIRTY-FOURTH SOUTHEASTERN SYMPOSIUM ON SYSTEM THEORY, 2002, : 81 - 85
  • [32] Dynamic Integral Sliding Mode for Launch Vehicle Attitude Control System
    Wang, Zirui
    Liu, Lei
    Wang, Yongji
    Wang, Zhishen
    PROCEEDINGS OF THE 2012 24TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2012, : 1713 - 1718
  • [33] Robust launch vehicle's generalized dynamic inversion attitude control
    Ansari, Uzair
    Bajodah, Abdulrahman H.
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2017, 89 (06): : 902 - 910
  • [34] Design and Implementation of Continuous Bounded Finite-Time Attitude Control of Reusable Launch Vehicle
    Li, Zhiyu
    Tian, Bailing
    Zhang, Xiuyun
    Zong, Qun
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2024, 71 (02) : 1917 - 1926
  • [35] Inverse Optimal Control Via Diagonal Stabilization Applied to Attitude Tracking of a Reusable Launch Vehicle
    Parvathy, Prasanna
    Jacob, Jeevamma
    JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS, 2021, 191 (2-3) : 794 - 822
  • [36] Inverse Optimal Control Via Diagonal Stabilization Applied to Attitude Tracking of a Reusable Launch Vehicle
    Prasanna Parvathy
    Jeevamma Jacob
    Journal of Optimization Theory and Applications, 2021, 191 : 794 - 822
  • [37] Real-Time Trajectory and Attitude Coordination Control for Reusable Launch Vehicle in Reentry Phase
    Tian, Bailing
    Fan, Wenru
    Su, Rui
    Zong, Qun
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2015, 62 (03) : 1639 - 1650
  • [38] Projective synchronization of a class of complex-variable chaotic systems by the UDE-based dynamic control method
    Zhang, Yaru
    Sun, Zuosheng
    Guo, Rongwei
    PROCEEDINGS OF THE 33RD CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2021), 2021, : 5697 - 5700
  • [39] Adaptive Control for Lateral Motion of Reusable Launch Vehicle Using Retrospective Cost Estimator
    Dai, Shicong
    Liu, Quanjun
    Wang, Ying
    Ren, Zhang
    Wang, Yudong
    Min, Changwan
    PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 3565 - 3569
  • [40] Adaptive Neural Network Fault Tolerant Control of Launch Vehicle Attitude System
    Ma, Yan-Ru
    Shi, Xiao-Rong
    Liu, Hua-Hua
    Liang, Xiao-Hui
    Wang, Qing
    Yuhang Xuebao/Journal of Astronautics, 2021, 42 (10): : 1237 - 1245