agile missile

基本解釋

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.
為研究具有大離軸角及越肩發(fā)射能力的先進(jìn)空空導(dǎo)彈初始段敏捷轉(zhuǎn)彎方法，研究了裝有反作用噴氣控制系統(tǒng)的空空導(dǎo)彈的大角度姿態(tài)過(guò)失速機(jī)動(dòng)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(dǎo)作戰(zhàn)模型考慮為一類(lèi)非線性、非高斯追逃攔截問(wèn)題，建立了噪聲環(huán)境中追逐-逃逸對(duì)策模型；
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