Modeling and Fixed-time Prescribed Performance Control for Hypersonic Morphing Vehicle

被引:0
|
作者
Cao C.-Y. [1 ]
Li F.-B. [1 ]
Liao Y.-X. [1 ]
Yin Z.-Y. [1 ]
Gui W.-H. [1 ]
机构
[1] School of Automation, Central South University, Changsha
来源
基金
中国国家自然科学基金;
关键词
disturbance observer; dynamic surface control; fixed-time; Hypersonic morphing vehicle; prescribed performance;
D O I
10.16383/j.aas.c230240
中图分类号
学科分类号
摘要
Taking a folding hypersonic morphing vehicle (HMV) as the research object, comprehensively considering dynamic changes caused by the deformation of aerodynamic characteristics and kinetics characteristics, as well as the influence of model uncertainties and external disturbances, the research on vehicle motion modeling and fixed-time prescribed performance control method is carried out. Firstly, the motion model and attitude control model of hypersonic morphing vehicle are established. Then, a fixed-time disturbance observer is established to accurately estimate the complex disturbance composed of model uncertainties and external disturbances, a novel fixed-time prescribed performance function is designed to quantitatively describe the expected performance constraints, the attitude controller is designed by integrating the dynamic surface control technique into the prescribed performance control framework, and the fixed-time stability of the closed-loop system is proved by Lyapunov stability theory. Finally, the numerical simulation is carried out to verify the effectiveness and robustness of the proposed method. © 2024 Science Press. All rights reserved.
引用
收藏
页码:486 / 504
页数:18
相关论文
共 32 条
  • [1] Song Hui-Xin, Jin Lei, Dynamic modeling and stability control of folding wing aircraft, Chinese Journal of Theoretical and Applied Mechanics, 52, 6, pp. 1548-1559, (2020)
  • [2] Zhang Yuan, Huang Wan-Wei, Lu Kun-Feng, Bai Wen-Yan, Yu Jiang-Long, Modeling and finite-time control for hypersonic morphing flight vehicle, Journal of Beijing University of Aeronautics and Astronautics, 48, 10, pp. 1979-1993, (2022)
  • [3] Bao C Y, Wang P, He R Z, Tang G J., Observer-based optimal control method combination with event-triggered strategy for hypersonic morphing vehicle, Aerospace Science and Technology, 136, (2023)
  • [4] Liang X H, Wang Q, Xu B, Dong C Y., Back-stepping fault-tolerant control for morphing aircraft based on fixed-time observer, International Journal of Control, Automation and Systems, 19, 12, pp. 3924-3936, (2021)
  • [5] Zhang Kang-Kang, Zhou Bin, Cai Guang-Bin, Hou Ming-Zhe, Prescribed-time tracking control of hypersonic vehicles by time-varying high-gain feedback, Acta Automatica Sinica
  • [6] Bu X W, Jiang B X, Lei H M., Nonfragile quantitative prescribed performance control of waverider vehicles with actuator saturation, IEEE Transactions on Aerospace and Electronic Systems, 58, 4, pp. 3538-3548, (2022)
  • [7] Ding Y B, Yue X K, Chen G S, Si J S., Review of control and guidance technology on hypersonic vehicle, Chinese Journal of Aeronautics, 35, 7, (2022)
  • [8] Tian B L, Li Z Y, Zhao X P, Zong Q., Adaptive multivariable reentry attitude control of RLV with prescribed performance, IEEE Transactions on Systems, Man, and Cybernetics: Systems, 52, 10, pp. 6674-6678, (2022)
  • [9] Luo Shi-Bin, Wu Xia, Wei Cai-Sheng, A novel attitude tracking control with guaranteed performance for reusable launch vehicle, Acta Aeronautica et Astronautica Sinica, 42, 11, pp. 415-426, (2021)
  • [10] Wang F, Wen L Z, Zhou C, Hua C H., Adaptive preassigned-time controller design for a hypersonic vehicle with improved performance and uncertainties, ISA Transactions, 132, pp. 309-328, (2023)