侧向射流推力器控制的大气拦截弹改道能力分析

Yu Yao, Yongtao Bi, Yuhang Wang
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引用次数: 0

摘要

为了分析侧向射流推进器控制的大气拦截弹的改道能力,建立了姿态控制型和改道型两种大气拦截弹的模型。考虑过载响应时间、推进器消耗和剩余时间,给出了在多种飞行条件下跟踪阶跃输入的最大末端改道距离。最后,在上述结果的基础上,考虑两种具有典型参数的导弹,给出了其相应的作战空域,并给出了其改道能力的发挥空间。
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Analysis of the divert ability of atmospheric interceptors controlled by lateral jet thrusters
In order to analyze the divert ability of atmospheric interceptors controlled by lateral jet thrusters, the models of two kinds of atmospheric interceptors are established: one is with attitude control thrusters, the other is with divert thrusters. Considering overload response time, consumptions of thrusters and time-to-go, maximal terminal divert distances are formulated for tracking a step input under several flight conditions. Finally, based on the above results, considering two types of missiles with typical parameters, their corresponding battle skies, where their divert abilities can be utilized, are given.
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