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未知攻击意图下目标—攻击者—防御者三方航天器博弈的容错控制策略设计-自主智能无人系统专刊

许宇航1,任清清1,孙靖华1,姜斌2,黄盘兴3   

  1. 1. 南京航空航天大学
    2. 南京航空航天大学自动化学院
    3. 哈尔滨工业大学
  • 收稿日期:2026-06-01 修回日期:2026-09-09 出版日期:2026-09-20 发布日期:2026-09-20
  • 通讯作者: 姜斌
  • 基金资助:
    国家自然科学基金;江苏省自然科学基金;空间智能控制技术全国重点实验室开放课题;中国航空学会青年科学家基金(制导导航与控制专项);直升机旋翼动力学国家级重点实验室开放基金;直升机旋翼动力学国家级重点实验室特别基金

Fault-tolerant control strategy design for target-attacker-defender three-sided spacecrafts game under unknown attacker intention

  • Received:2026-06-01 Revised:2026-09-09 Online:2026-09-20 Published:2026-09-20
  • Supported by:
    National Natural Science Foundation of China;Natural Science Foundation of Jiangsu Province of China;Open fund of the Science and Technology on Space Intelligent Control Laboratory under Grant;CSAA Youth Scientist Fund (Guidance, Navigation, and Control);Open fund of the National Key Laboratory of Helicopter Aeromechanics;Special fund of the National Key Laboratory of Helicopter Aeromechanics

摘要: 针对航天器目标-攻击者-防御者三方博弈中攻击意图未知且防御航天器存在执行器故障的问题,提出一种融合自适应估计与微分博弈的协同容错控制方法,实现对目标的高效保护。考虑目标沿任意轨迹运动及目标主动逃逸两种典型场景,首先利用自适应估计理论设计故障估计律,在线辨识防御航天器的执行器故障。在此基础上,针对不同场景分别构造复合学习律,在线学习并预测攻击航天器的控制增益矩阵,进而量身定制防御航天器的最优容错控制策略。该策略只需满足区间激励条件,无需持续激励,降低计算负担,节省星上资源。理论分析表明,所设计的三方博弈策略达到-纳什均衡,实现在估计误差影响下的近似均衡性。最后,通过仿真结果验证所设计的容错博弈方法能有效预判攻击航天器的意图并实施拦截,从而保护目标航天器。

关键词: 轨道博弈, 执行器故障, 容错控制, 自适应估计, 意图识别, ε-纳什均衡

Abstract: To address the issues of unknown attack intent and actuator faults in the defender spacecraft within a target-attacker-defender three-party game, this paper proposes a cooperative fault-tolerant control method that integrates adaptive estimation and differential game theory to achieve efficient protection of the target. Two typical scenarios are considered: the target moving along an arbitrary trajectory and the target actively evading. First, an adaptive estimation law is designed using adaptive estimation theory to online identify actuator faults in the defender spacecraft. On this basis, composite learning laws are constructed for the two scenarios to enable the defender spacecraft to learn and predict the control gain matrix of the attacker online, and subsequently tailor the optimal fault-tolerant control strategy for the defender. The proposed strategy only requires interval excitation condition rather than persistent excitation, thereby reducing computational burden and saving onboard resources. Theoretical analysis shows that the designed three-party game strategy achieves an -Nash equilibrium, ensuring approximate equilibrium under the influence of estimation errors. Finally, simulation results demonstrate that the proposed fault-tolerant game method can effectively predict the attacker's intent and perform interception, thereby protecting the target spacecraft.

Key words: Orbital game, actuator fault, fault-tolerant control, adaptive estimation, intent recognition, ε-Nash equilibrium

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