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Guidance Law Design For Two Flight Vehicles Cooperative Interception

机译:两架飞行器协同拦截的制导律设计

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In this paper, we consider the guidance law design problem for two fight vehicles cooperatively intercepting a maneuvering target. The aim of cooperative interception is to improve the hit-to-kill accuracy under large detection noises. We first formulate the cooperative interception problem into a stochastic control model without assuming that the Separation Theorem is holding, and a terminal miss distance is defined for the two intercepting flight vehicles cooperative interception. Moreover, the Probability Density Function (PDF) of the defined terminal miss distance is calculated. Then, by minimizing the expectation of the defined terminal miss distance, the optimal positions of the intercepting flight vehicles are obtained and the control law is designed based on the optimal control theory. Last, simulation experiments are carried out to illustrate the effectiveness of the proposed approach.
机译:在本文中,我们考虑了两个战斗机协同拦截机动目标的制导律设计问题。协同拦截的目的是提高大检测噪声下的击杀准确性。我们首先将协作拦截问题公式化为随机控制模型,而无需假设分离定理成立,并且为两个拦截飞行器的协作拦截定义了末尾未命中距离。此外,计算定义的终端未命中距离的概率密度函数(PDF)。然后,通过最小化定义的终端失误距离的期望,获得拦截飞行器的最优位置,并基于最优控制理论设计控制律。最后,进行了仿真实验以说明所提方法的有效性。

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