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Finite-time stability analysis of proportional navigation guidance system

机译:比例导航制导系统的有限时稳定性分析

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The finite time stability of proportional navigation guidance system is presented. A linearized proportional navigation guidance loop is introduced. The reassembled model of guidance loop exhibits a famous Lur''e system which consisting of a linear time-invariant element and a time-varying part. It is shown that a sufficient condition for stability, with 1≤p≤∞, is obtained by utilizing the well-known small gain theorem. Based on the condition of system stability, the relation between guidance loop stability and miss distance is proved. It is proved that, if the linear time-invariant part of the system belongs to the class of positive real transfer functions, the guidance system is stable and the guidance system can achieve zero miss distance.
机译:提出了比例导航制导系统的时间稳定性。引入了线性比例导航制导环。引导环的重新组装模型展示了著名的Lur'e系统,该系统由线性时不变元素和时变部分组成。结果表明,利用众所周知的小增益定理可以得到1≤p≤∞的充分稳定性条件。根据系统稳定性的条件,证明了制导环的稳定性与脱靶距离之间的关系。证明了,如果系统的线性时不变部分属于正实传递函数类,则制导系统是稳定的,制导系统可以实现零失误距离。

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