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基于追逃博弈的非合作目标接近控制
引用本文:柴源,罗建军,王明明,韩楠. 基于追逃博弈的非合作目标接近控制[J]. 宇航总体技术, 2020, 4(1): 30-38
作者姓名:柴源  罗建军  王明明  韩楠
作者单位:西北工业大学航天飞行动力学技术重点实验室; 西北工业大学青岛研究院,西北工业大学航天飞行动力学技术重点实验室; 西北工业大学青岛研究院,西北工业大学航天飞行动力学技术重点实验室; 西北工业大学青岛研究院,西北工业大学航天飞行动力学技术重点实验室; 西北工业大学青岛研究院
基金项目:国家自然科学基金重大项目(61690210,61690211);青岛市源头创新计划(18-2-2-14-jch)
摘    要:针对追踪航天器接近非合作目标任务中的相对位置控制问题,提出了一种基于线性二次型追逃博弈的控制方法。首先,将非合作目标接近问题转化为二人追逃博弈问题,并设计了二次型目标函数。其次,结合相对运动模型,建立了线性二次型追逃博弈模型。为得到纳什均衡策略,将HJ方程转化为代数黎卡提方程,并给出了李雅普诺夫迭代法对其求解。最后,对博弈控制方法的有效性进行仿真验证,结果表明,该方法能够在非合作目标机动时实现轨道接近控制。

关 键 词:相对运动;追逃博弈;非合作目标

Pursuit-Evasion Game Control for Approaching Space Non-Cooperative Target
CHAI Yuan,LUO Jianjun,WANG Mingming and HAN Nan. Pursuit-Evasion Game Control for Approaching Space Non-Cooperative Target[J]. Astronautical Systems Engineering Technology, 2020, 4(1): 30-38
Authors:CHAI Yuan  LUO Jianjun  WANG Mingming  HAN Nan
Affiliation:National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University; Qingdao Research Institute, Northwestern Polytechnical University,National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University; Qingdao Research Institute, Northwestern Polytechnical University,National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University; Qingdao Research Institute, Northwestern Polytechnical University and National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University; Qingdao Research Institute, Northwestern Polytechnical University
Abstract:A linear quadratic differential game control method based on pursuit-evasion game theory is proposed for a chasing spacecraft approaching a non-cooperative target. Firstly, based on the analysis of approaching non-cooperative target, the relative orbit control problem is formulated into a two-player pursuit-evasion game. According to the control requirements of optimal consumption and high-accuracy approaching, the quadratic performance index function is designed. Secondly, combining the linearized relative motion model between chasing spacecraft and non-cooperative target, a linear quadratic pursuit-evasion game model is established. Then, the HJ equation is transformed into algebra Riccati equations which can be solved by Lyapunov iterations to get the Nash equilibrium strategy. Finally, the simulation results show that the linear quadratic pursuit-evasion control can achieve orbital proximity even if the non-cooperative target maneuvers.
Keywords:Relative orbit motion   Pursuit-evasion game   Non-cooperative target
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