考虑测量误差的高超声速飞行器抗干扰追逃博弈OA
Anti-disturbance pursuit-evasion game for hypersonic vehicles under measurement errors
高超声速飞行器在空天对抗中具有重要的战略价值,但日益发展的拦截技术和复杂的对抗环境干扰给飞行器规避策略设计带来巨大挑战.针对由传感器测量引入的相对距离、纵向视线角及侧向视线角3类测量误差下的高超声速飞行器追逃博弈问题,提出了一种双层抗干扰博弈规避控制架构.首先,根据攻防双方的运动方程,构建相对运动学模型和零和微分博弈模型,并对上述测量误差进行建模与表征.其次,在控制层设计基于非线性自适应观测器的抗干扰控制算法,补偿测量误差对系统的影响.接着,在博弈决策层制定追逃飞行器的性能指标函数,通过求解相关的HJI方程推导出最优规避策略,并采用自适应动态规划技术,利用评价神经网络来近似该最优策略.最后,通过多场景数值仿真与蒙特卡洛仿真验证了所提方法的有效性与鲁棒性,分析了规避效果对3类测量误差的灵敏度,结果表明该方法能有效提升高超声速飞行器在测量误差下的规避性能.
Hypersonic Hight vehicles have important strategic value in aerospace confrontation.However,the rapidly developing interception technologies and complex disturbance in adversarial environments pose great challenges to the design of evasion strategies for such vehicles.Aiming at the pursuit-evasion game problem of hypersonic Hight ve-hicles under three types of sensor measurement errors,namely relative distance,longitudinal line-of-sight angle and lateral line-of-sight angle,this paper proposes a dual-layer anti-disturbance game-based evasion control framework.First,based on the motion equations of both the attacker and defender,a relative kinematic model and a zero-sum dif-ferential game model are established,and the above measurement errors are modeled and characterized.Second,at the control layer,an anti-disturbance control algorithm based on a nonlinear adaptive observer is designed to compen-sate for the influence of measurement errors on the system.Then,at the game decision-making layer,a performance index function for the pursuit-evasion vehicles is developed.The optimal evasion strategy is derived by solving the cor-responding Hamilton-Jacobi-Isaacs(HJI)equation,and adaptive dynamic programming is adopted to approximate the optimal strategy using a critic neural network.Finally,multi-scenario numerical simulations and Monte Carlo simula-tions are carried out to verify the effectiveness and robustness of the proposed method.The sensitivity of evasion per-formance to the three types of measurement errors is analyzed.The results demonstrate that the proposed method can effectively improve the evasion performance of hypersonic vehicles under measurement errors.
张泽君;王恩美;陈泽帅;李晨龙;章健淳;余翔
北京航空航天大学 杭州创新研究院,杭州 310051北京航空航天大学 杭州创新研究院,杭州 310051北京航空航天大学 自动化科学与电气工程学院,北京 100191北京航空航天大学 杭州创新研究院,杭州 310051北京航空航天大学 杭州创新研究院,杭州 310051北京航空航天大学 杭州创新研究院,杭州 310051||北京航空航天大学 自动化科学与电气工程学院,北京 100191
航空航天
高超声速飞行器追逃博弈抗干扰控制零和微分博弈自适应动态规划
hypersonic flight vehiclepursuit-evasion gameanti-disturbance controlzero-sum differential gameadaptive dynamic programming
《航空学报》 2026 (9)
68-85,18
国家自然科学基金(62403039,62595803,62573033,62573034,62473031) National Natural Science Foundation of China(62403039,62595803,62573033,62573034,62473031)
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