Data-Driven Based Model-Free Adaptive Optimal Control Method for Hypersonic Morphing Vehicle

被引:14
作者
Bao, Cunyu [1 ]
Wang, Peng [1 ]
Tang, Guojian [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China
关键词
Aerodynamics; Adaptation models; Optimal control; Attitude control; Steady-state; Vehicle dynamics; Uncertainty; ROBUST TRACKING CONTROL; DISTURBANCE OBSERVER; DESIGN; APPROXIMATION; STABILIZATION; UNCERTAINTIES; SYSTEMS; INPUT; UAV;
D O I
10.1109/TAES.2022.3230633
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Aiming at the attitude control of a class of hypersonic morphing vehicles (HMVs) with variable sweep wings, a model-free adaptive dynamic planning (MFADP) optimal control method based on data-driven and finite-time fuzzy disturbance observer is proposed in this article. An integrated oriented-control attitude-morphing model is established, and morphing is considered as the state to carry out the integrated coupling attitude control. The control scheme is organized by a steady-feedback-compensation framework. To overcome the dependence on the unknown dynamic knowledge of HMVs, the dynamic model is reconstructed using neural networks for steady-state control. Subsequently, based on the MFADP algorithm, an Off-On serial policy learning strategy is designed for the error model to obtain a real-time approximate optimal feedback control. Additionally, a fuzzy disturbance observer with finite-time convergence ability is proposed to estimate and compensate the multiple uncertainties. Finally, the stability of the closed-loop system is proved theoretically and the simulation results demonstrate the improved performance of the proposed method.
引用
收藏
页码:3713 / 3725
页数:13
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