发明名称 SYSTEM FOR CORRECTING THE TRAJECTORY OF A MISSILE
摘要 <p>System for correcting the trajectory of a missile, in particular a shell, to ensure it attains the specified target. The system comprises an optical radar (10) with a laser (16) emitting in the infrared range, which, in conjunction with a processing device (11), makes it possible to follow at the same time the movements of the target and missile. The information supplied by the processing device (11) are used for calculating in a computer (9) the corrections to be made to the trajectory of the missile (2) in a final phase, to ensure it hits the target (4). The invention is applicable to systems for controlling the firing of shells and self-propelled missiles.</p>
申请公布号 WO1989007744(A1) 申请公布日期 1989.08.24
申请号 FR1989000060 申请日期 1989.02.17
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