agile missile

基本解释

This paper investigates the large angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
爲研究具有大離軸角及越肩發射能力的先進空空導彈初始段敏捷轉彎方法，研究了裝有反作用噴氣控制系統的空空導彈的大角度姿態過失速機動控制律。
First, based on the consideration that the model for anti-missiles is a nonlinear and non-Gaussian problem, a model is built of guiding a missile towards an evading agile target in noisy environments.
首先，將攔截器反導作戰模型考慮爲一類非線性、非高斯追逃攔截問題，建立了噪聲環境中追逐-逃逸對策模型；
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