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DOI:
飞控与探测:2025,8(6):27-36
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基于KOA算法的航天器连续推力追逃防博弈策略设计
(1.南京航空航天大学 航天学院;2.马鞍山学院;3.中国航天科技体系与创新研究院)
Design of Spacecraft Continuous Thrust Pursuit-Escape- Defense Game Strategy Based on KOA Algorithm
(1.School of Astronautics, Nanjing University of Aeronautics and Astronautics;2.Maanshan College;3.China Aerospace Science and Technology System and Innovation Research Institute)
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中文摘要: 针对追击-逃逸-防御三方航天器博弈对抗问题,提出了基于开普勒优化算法(Kepler Optimization Algorithm,KOA)求解连续推力追逃防博弈对抗问题的方法。在微分对策理论基础上,建立了动力学模型和博弈控制模型,设计博弈控制过程的优化变量和目标函数。进一步考虑有防御航天器的实际场景,通过仿真验证,结果表明,利用KOA 算法在处理动态博弈问题时独特的迭代机制和高效的搜索能力,能够有效求解连续推力追逃防博弈对抗问题。
Abstract:Aiming at the three-body spacecraft pursuit-escape-defense game confrontation problem, a method based on the Kepler optimization algorithm (KOA) is proposed to solve the continuous thrust pursuit-escape defense game confrontation problem. Based on the differential game theory, the dynamic model and game control model are established, and the optimization variables and objective functions of the game control process are designed. Further considering the actual scenario of defensive spacecraft, the simulation results show that the KOA algorithm can effectively solve the continuous thrust pursuit-escape defense game confrontation problem by utilizing its unique iterative mechanism and efficient search ability in dealing with dynamic game problems.
文章编号:20250603     中图分类号:V448.2;V412.4    文献标志码:A
基金项目:微小型航天器快速设计与智能集群全国重点实验室基金(MS01240109);南京航空航天大学科研与实践创新计划(xcxjh20241504)
引用文本:
尹兴,贾庆贤,孙秀芹,侍野,陈可羽.基于KOA算法的航天器连续推力追逃防博弈策略设计[J].飞控与探测,2025,8(6):27-36.