会合
微分博弈
卫星
轨道(动力学)
计算机科学
差速器(机械装置)
启发式
椭圆轨道
航空航天工程
模拟
数学优化
航天器
物理
工程类
数学
人工智能
经典力学
作者
Eric R. Prince,Joshuah A. Hess,Richard Cobb,Ryan Carr
出处
期刊:Journal of Guidance Control and Dynamics
[American Institute of Aeronautics and Astronautics]
日期:2019-07-01
卷期号:42 (7): 1458-1472
被引量:17
摘要
Differential games are formulated and solved for an inspector satellite operating nearby a resident space object (RSO) in an elliptical orbit. For each differential game, the goal of the inspector satellite is to minimize the time to achieve an inspection goal, whereas the goal of the RSO is to delay that condition as long as possible. Thus, it is assumed that the RSO can maneuver, and that both the inspector satellite and the RSO use a constant, steerable thruster (for example, an electric engine) during each game. The following games are formulated and solved via an indirect heuristic method, where each game corresponds to an inspection goal of the inspector satellite: 1) intercept; 2) rendezvous; 3) obtain sun vector; 4) match energy; 5) obtain sun vector and match energy; and 6) match energy and remain in close proximity during the ensuing orbit. The open-loop strategies obtained for these games represent worst-case scenarios, and they may inform requirements for future satellites as well as be actual open-loop strategies for a given scenario.
科研通智能强力驱动
Strongly Powered by AbleSci AI