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本文主要是围绕研究拦截导弹的直接力的控制与制导所展开的,研究了直接里拦截导弹的模型。通过导弹在三维空间的位置及其运动规律的描述,建立了空间追逃问题的数学问来实现拦截导弹的功能。并通过有关的数学模型及相关坐标表示(转换)实现拦截导弹的智能化控制。本文还研究了拦截导弹的制导的误差来源。建立了空间追逃问题的数学问来实现拦截导弹的功能。最终实现导弹的高校、智能、精确控制。
This paper mainly focuses on the control and guidance of studying the direct force of interceptor missiles, and studies the model of interceptor missiles directly. Through the description of the missile’s position in the three-dimensional space and its movement law, the mathematical problem of space pursuit is established to realize the function of interceptor missile. And through the relevant mathematical model and related coordinate representation (conversion) to achieve the intelligent control of interceptor missiles. The paper also studies the sources of error in the guidance of interceptor missiles. The establishment of a mathematical pursuit of space pursuit problem to achieve interceptor missile function. The ultimate realization of missile colleges and universities, intelligent, precise control.