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以高空动能拦截器为研究对象 ,为其末制导段设计了一种“逐段限制视线转率”的导引方法 ,使之最终能直接命中目标 ,实现动能拦截的任务并通过仿真计算验证了该导引法的可行性。
Taking the high-altitude kinematic interceptor as the research object, a guide-line method of “limiting the line-of-sight line-by-line” was designed for the final guidance section so as to finally hit the target directly and realize the task of kinetic energy interception. The feasibility of this guidance method.