An AutoML based trajectory optimization method for long-distance spacecraft pursuit-evasion game

被引:0
|
作者
YANG Fuyunxiang [1 ]
YANG Leping [1 ]
ZHU Yanwei [1 ]
机构
[1] College of Aerospace Science and Engineering, National University of Defense Technology
关键词
D O I
暂无
中图分类号
O225 [对策论(博弈论)]; V52 [航天术];
学科分类号
070105 ; 08 ; 0825 ; 1201 ;
摘要
Current successes in artificial intelligence domain have revitalized interest in spacecraft pursuit-evasion game,which is an interception problem with a non-cooperative maneuvering target. The paper presents an automated machine learning(AutoML) based method to generate optimal trajectories in long-distance scenarios. Compared with conventional deep neural network(DNN) methods, the proposed method dramatically reduces the reliance on manual intervention and machine learning expertise. Firstly, based on differential game theory and costate normalization technique, the trajectory optimization problem is formulated under the assumption of continuous thrust. Secondly, the AutoML technique based on sequential model-based optimization(SMBO) framework is introduced to automate DNN design in deep learning process. If recommended DNN architecture exists, the tree-structured Parzen estimator(TPE) is used, otherwise the efficient neural architecture search(NAS) with network morphism is used. Thus, a novel trajectory optimization method with high computational efficiency is achieved. Finally, numerical results demonstrate the feasibility and efficiency of the proposed method.
引用
收藏
页码:754 / 765
页数:12
相关论文
共 50 条
  • [1] An AutoML based trajectory optimization method for long-distance spacecraft pursuit-evasion game
    Yang, Fuyunxiang
    Yang, Leping
    Zhu, Yanwei
    JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2023, 34 (03) : 754 - 765
  • [2] A Fuel Optimization Method for the Pursuer in the Spacecraft Pursuit-Evasion Game
    Wang, Qi-shuai
    Li, Pei
    Lei, Ting
    Liu, Xiao-feng
    Cai, Guo-ping
    JOURNAL OF COMPUTATIONAL AND NONLINEAR DYNAMICS, 2022, 17 (07):
  • [3] Comparison of Two Optimal Guidance Methods for the Long-Distance Orbital Pursuit-Evasion Game
    Zeng, Xin
    Yang, Leping
    Zhu, Yanwei
    Yang, Fuyunxiang
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2021, 57 (01) : 521 - 539
  • [4] Situation analysis method based on level set for spacecraft pursuit-evasion game
    Yang F.
    Yang L.
    Zhu Y.
    Zhang C.
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2024, 46 (03): : 30 - 38
  • [5] Intercepting a Superior Missile: Trajectory Optimization Approach to a Pursuit-Evasion Game
    Altaher, Mohammad
    Nomir, Omaima
    ElMougy, Samir
    INTERNATIONAL GAME THEORY REVIEW, 2020, 22 (04)
  • [6] Method of spacecraft cluster orbital pursuit-evasion game based on the hierarchical theory structure
    Feng, Haolong
    Wu, Songtai
    Liu, Shengyang
    Song, Ting
    Han, Fei
    2024 3RD CONFERENCE ON FULLY ACTUATED SYSTEM THEORY AND APPLICATIONS, FASTA 2024, 2024, : 438 - 442
  • [7] Guidance strategy of motion camouflage for spacecraft pursuit-evasion game
    Jianqing LI
    Chaoyong LI
    Yonghe ZHANG
    Chinese Journal of Aeronautics, 2024, (03) : 312 - 319
  • [8] Guidance strategy of motion camouflage for spacecraft pursuit-evasion game
    Li, Jianqing
    Li, Chaoyong
    Zhang, Yonghe
    CHINESE JOURNAL OF AERONAUTICS, 2024, 37 (03) : 312 - 319
  • [9] Guidance strategy of motion camouflage for spacecraft pursuit-evasion game
    LI, Jianqing
    LI, Chaoyong
    ZHANG, Yonghe
    Chinese Journal of Aeronautics, 1600, 37 (03): : 312 - 319
  • [10] A DIMENSION-REDUCTION METHOD FOR THE FINITE-HORIZON SPACECRAFT PURSUIT-EVASION GAME
    Qi-Shuai Wang
    Li, Pei
    Lei, Ting
    Xiao-Feng Liu
    Guo-Ping Cai
    JOURNAL OF INDUSTRIAL AND MANAGEMENT OPTIMIZATION, 2023, 19 (03) : 1983 - 1998