Optimal delta-V-based strategies in orbital pursuit-evasion games

被引:17
作者
Han, Hongyu [1 ]
Dang, Zhaohui [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Peoples R China
[2] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
Evasion maneuver; Non -cooperative target; Orbital pursuit -evasion; Two -point boundary value problem;
D O I
10.1016/j.asr.2023.03.028
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This research investigates the orbital pursuit-evasion games with impulsive maneuvers in long-distance interception scenarios. Specifically, this paper examines the influences of escape impulses, with different directions, applied by the evader on the intercept-correction delta-v (DVCorr) of the pursuer that is already on an interception orbit. After obtaining the evader's strategies based on maximizing the DVCorr under different circumstances, it is found that, with the knowledge of the evader's best strategy, the pursuer could make DVCorr smaller by adjusting its initial interception orbit. Then, a method to modify the initial orbit with energy constraints is designed so that the pursuer can match the evader's escape maneuver with less delta-v to prepare. Finally, this paper summarizes the best strategies of both sides after considering the initial trajectory adjustment and discusses the impact of incomplete information on tactics in orbital pursuitevasion games.& COPY; 2023 COSPAR. Published by Elsevier B.V. All rights reserved.
引用
收藏
页码:243 / 256
页数:14
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