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Cooperative Guidance Strategies for Aircraft Defence with Impact Angle Constraints

机译:冲击角约束的飞机防御协同制导策略

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A differential game based cooperative guidance strategy is proposed for the active-aircraft defence from an attacking interceptor, where the target aircraft actively protects itself by launching a defending interceptor to intercept the attacking interceptor. To increase the effectiveness of the defending interceptor, the proposed guidance strategy also imposes an impact angle constraint at the time of interception with negligible miss distance. The three-body pursuit-evasion problem is formulated as a linear quadratic differential game (LQDG) problem. Firstly, a general form of the cooperative guidance strategy for the linear quadratic differential game is presented. Then an analytic solution of LQDG is derived for a case of zero-lag dynamics of the adversaries. Finally, numerical simulations are carried out for several test cases to evaluate the performance of the proposed cooperative guidance strategy.
机译:提出了一种基于差分博弈的协同制导策略,用于攻击拦截机对主动飞机的防御,目标飞机通过发射防御拦截机来拦截攻击拦截机,从而主动地保护自身。为了提高防御拦截器的效率,所提出的制导策略还对拦截时的撞击角施加了可忽略的错过距离约束。三体追逃问题被公式化为线性二次微分对策(LQDG)问题。首先,提出了线性二次微分博弈的合作制导策略的一般形式。然后,针对敌手零滞后动力学的情况,导出了LQDG的解析解。最后,针对几个测试案例进行了数值模拟,以评估所提出的合作制导策略的性能。

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