Flight Control of Waverider Vehicles With Fragility-Avoidance Prescribed Performance

被引:58
作者
Bu, Xiangwei [1 ]
Hua, Changchun [2 ]
Lv, Maolong [3 ]
Wu, Zhonghua [4 ]
机构
[1] Air Force Engn Univ, Air & Missile Def Coll, Xian 710051, Peoples R China
[2] Yanshan Univ, Sch Elect Engn, Qinhuangdao 066004, Peoples R China
[3] Air Force Engn Univ, Coll Air Traff Control & Nav, Xian 710051, Peoples R China
[4] Henan Polytech Univ, Sch Elect Engn & Automat, Jiaozuo 454000, Peoples R China
关键词
Vehicle dynamics; Protocols; Force; Uncertainty; Transient analysis; Steady-state; Fluctuations; Flexible prescribed funnel; fragility-avoidance; fuzzy neural approximation; prescribed performance control (PPC); waverider vehicles (WVs); ATTITUDE-TRACKING CONTROL; FAULT-TOLERANT CONTROL; RIGID SPACECRAFT; FEEDBACK; SYSTEMS;
D O I
10.1109/TAES.2023.3251314
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article proposes a prescribed performance control (PPC) methodology called fragility-avoidance PPC for waverider vehicles (WVs) with sudden disturbances based on fuzzy neural approximation. We raise the fragile problem associated with the existing PPC, and to remedy this defect, we construct a flexible prescribed funnel that is able to sense the error fluctuation caused by sudden disturbances and, moreover, tackle the fragile problem by automatically adjusting prescribed boundaries. Then, a simplified fuzzy neural approximation framework is presented to reject the unknown nonaffine dynamics of WVs while avoiding the algebraic loop problem. The stability of the closed-loop system is proved via the Lyapunov method, and finally, the effectiveness and superiority of the addressed method are verified by compared simulations.
引用
收藏
页码:5248 / 5261
页数:14
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  • [11] Approximation-Free Control for Vehicle Active Suspensions With Hydraulic Actuator
    Huang, Yingbo
    Na, Jing
    Wu, Xing
    Gao, Guanbin
    [J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2018, 65 (09) : 7258 - 7267
  • [12] Fuzzy adaptive observer-based fault estimation design with adjustable parameter for satellite under unknown actuator faults and perturbations
    Li, Yanbo
    Xu, Wei
    Chang, Lin
    [J]. IET CONTROL THEORY AND APPLICATIONS, 2022, 16 (08) : 741 - 761
  • [13] Appointed-time fault-tolerant attitude tracking control of spacecraft with double-level guaranteed performance bounds
    Liu, Mingmin
    Shao, Xiaodong
    Ma, Guangfu
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 : 337 - 346
  • [14] Constrained Attitude Control of Uncertain Spacecraft With Appointed-Time Control Performance
    Lu, Xuhui
    Jia, Yingmin
    Fu, Yongling
    Matsuno, Fumitoshi
    [J]. IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2023, 53 (01): : 178 - 190
  • [15] Robust inertia-free attitude takeover control of postcapture combined spacecraft with guaranteed prescribed performance
    Luo, Jianjun
    Wei, Caisheng
    Dai, Honghua
    Yin, Zeyang
    Wei, Xing
    Yuan, Jianping
    [J]. ISA TRANSACTIONS, 2018, 74 : 28 - 44
  • [16] Low-complexity prescribed performance control for spacecraft attitude stabilization and tracking
    Luo, Jianjun
    Yin, Zeyang
    Wei, Caisheng
    Yuan, Jianping
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 74 : 173 - 183
  • [17] Adaptive Pose Control for Spacecraft Proximity Operations With Prescribed Performance Under Spatial Motion Constraints
    Shao, Xiaodong
    Hu, Qinglei
    Shi, Yang
    [J]. IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2021, 29 (04) : 1405 - 1419
  • [18] Inertia-free fault-tolerant spacecraft attitude tracking using control allocation
    Shen, Qiang
    Wang, Danwei
    Zhu, Senqiang
    Poh, Eng Kee
    [J]. AUTOMATICA, 2015, 62 : 114 - 121
  • [19] Adaptive state feedback and tracking control of systems with actuator failures
    Tao, G
    Joshi, SM
    Ma, XL
    [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2001, 46 (01) : 78 - 95
  • [20] Adaptive Attitude-Tracking Control of Spacecraft with Uncertain Time-Varying Inertia Parameters
    Thakur, Divya
    Srikant, Sukumar
    Akella, Maruthi R.
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (01) : 41 - 52