中国航空学报(英文版)2024,Vol.37Issue(5) :441-461.DOI:10.1016/j.cja.2024.02.024

A novel evasion guidance for hypersonic morphing vehicle via intelligent maneuver strategy

Xun LI Xiaogang WANG Hongyu ZHOU Yu LI
中国航空学报(英文版)2024,Vol.37Issue(5) :441-461.DOI:10.1016/j.cja.2024.02.024

A novel evasion guidance for hypersonic morphing vehicle via intelligent maneuver strategy

Xun LI 1Xiaogang WANG 1Hongyu ZHOU 1Yu LI2
扫码查看

作者信息

  • 1. Department of Aerodynamics,Harbin Institute of Technology,Harbin 150001,China
  • 2. Beijing Aerospace Technology Institute,Beijing 100074,China
  • 折叠

Abstract

This paper presents a novel evasion guidance law for hypersonic morphing vehicles,focusing on determining the optimized wing's unfolded angle to promote maneuverability based on an intelligent algorithm.First,the pursuit-evasion problem is modeled as a Markov decision process.And the agent's action consists of maneuver overload and the unfolded angle of wings,which is different from the conventional evasion guidance designed for fixed-shape vehicles.The reward function is formulated to ensure that the miss distances satisfy the prescribed bounds while minimizing energy consumption.Then,to maximize the expected cumulative reward,a residual learning method is proposed based on proximal policy optimization,which integrates the optimal evasion for linear cases as the baseline and trains to optimize the performance for nonlinear engage-ment with multiple pursuers.Therefore,offline training guarantees improvement of the constructed evasion guidance law over conventional ones.Ultimately,the guidance law for online implementa-tion includes only analytical calculations.It maps from the confrontation state to the expected angle of attack and the unfolded angle while retaining high computational efficiency.Simulations show that the proposed evasion guidance law can utilize the change of unfolded angle to extend the max-imum overload capability.And it surpasses conventional maneuver strategies by ensuring better evasion efficacy and higher energy efficiency.

Key words

Hypersonic vehicles/Variable-sweep wings/Evasion guidance/Reinforcement learning/Pursuit-evasion problem

引用本文复制引用

基金项目

National Natural Science Foundation of China(52202438)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
段落导航相关论文