Impulsive thrust strategy for orbital pursuit-evasion games based on impulse-like constraint

被引:2
作者
Wang, Hongbo [1 ]
Zhang, Yao [1 ]
Liu, Hao [2 ]
Zhang, Kunpeng [2 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
[2] Beijing Inst Control Engn, Natl Key Lab Space Intelligent Control, Beijing 100094, Peoples R China
关键词
Orbital pursuit-evasion game; Differential game; Impulsive thrust; Deep learning; Shooting method; GUIDANCE;
D O I
10.1016/j.cja.2024.08.011
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper proposes a novel impulsive thrust strategy guided by optimal continuous thrust strategy to address two-player orbital pursuit-evasion game under impulsive thrust control. The strategy seeks to enhance the interpretability of impulsive thrust strategy by integrating it within the framework of differential game in traditional continuous systems. First, this paper introduces an impulse-like constraint, with periodical changes in thrust amplitude, to characterize the impulsive thrust control. Then, the game with the impulse-like constraint is converted into the two-point boundary value problem, which is solved by the combined shooting and deep learning method proposed in this paper. Deep learning and numerical optimization are employed to obtain the guesses for unknown terminal adjoint variables and the game terminal time. Subsequently, the accurate values are solved by the shooting method to yield the optimal continuous thrust strategy with the impulse-like constraint. Finally, the shooting method is iteratively employed at each impulse decision moment to derive the impulsive thrust strategy guided by the optimal continuous thrust strategy. Numerical examples demonstrate the convergence of the combined shooting and deep learning method, even if the strongly nonlinear impulse-like constraint is introduced. The effect of the impulsive thrust strategy guided by the optimal continuous thrust strategy is also discussed. (c) 2024 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).
引用
收藏
页数:17
相关论文
共 40 条
[1]  
Aharonian F, 2020, Arxiv, DOI [arXiv:2010.06205, 10.3969/j.issn.1002-2481.2020.06.30, DOI 10.19641/J.CNKI.42-1290/F.2023.11.019]
[2]   BARRIER IN PURSUIT-EVASION PROBLEMS BETWEEN 2 LOW-THRUST ORBITAL SPACECRAFT [J].
ANDERSON, GM ;
GRAZIER, VW .
AIAA JOURNAL, 1976, 14 (02) :158-163
[3]   A tutorial on the deterministic Impulse Control Maximum Principle: Necessary and sufficient optimality conditions [J].
Chahim, Mohammed ;
Hartl, Richard F. ;
Kort, Peter M. .
EUROPEAN JOURNAL OF OPERATIONAL RESEARCH, 2012, 219 (01) :18-26
[4]   Linear-quadratic and norm-bounded differential game combined guidance strategy against active defense aircraft in three-player engagement [J].
Chao, Tao ;
Wang, Xintao ;
Wang, Songyan ;
Yang, Ming .
CHINESE JOURNAL OF AERONAUTICS, 2023, 36 (08) :331-350
[5]   OPTIMAL INTERCEPT GUIDANCE FOR SHORT-RANGE TACTICAL MISSILES [J].
COTTRELL, RG .
AIAA JOURNAL, 1971, 9 (07) :1414-&
[6]   Pursuit-evasion games with impulsive dynamics [J].
Cruck, Eva ;
Quincampoix, Marc ;
Saint-Pierre, Patrick .
ADVANCES IN DYNAMIC GAME THEORY: NUMERICAL METHODS, ALGORITHMS, AND APPLICATIONS TO ECOLOGY AND ECONOMICS, 2007, 9 :223-+
[7]  
Daughtery JA, 2020, dissertation
[8]   OPTIMUM INTERCEPT LAWS FOR ACCELERATING TARGETS [J].
GARBER, V .
AIAA JOURNAL, 1968, 6 (11) :2196-&
[9]   Sensitivity Methods Applied to Orbital Pursuit Evasion [J].
Hafer, William T. ;
Reed, Helen L. ;
Turner, James D. ;
Khanh Pham .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (06) :1118-U217
[10]   Models and Strategies for J2-Perturbed Orbital Pursuit-Evasion Games [J].
Han, Hongyu ;
Dang, Zhaohui .
SPACE-SCIENCE & TECHNOLOGY, 2023, 3