发明名称 IN-FLIGHT PROGRAMMING OF TRIGGER TIME OF A PROJECTILE
摘要 <p>The present invention describes methods for programming trigger time of a projectile (60) based on remaining flight time to a target (P) after the projectile (60) is airborne. The actual muzzle (Vo) and flight speeds (V1, V2, etc.) are independently determined and compared to those used by the ballistic computer (30), and a better estimate of trigger time is accordingly used to activate detonation of the projectile (60). In one embodiment, a Kalman algorithm is used to provide a better estimate of the projectile's flight speeds obtained by independent methods to provide the better estimate of the trigger time.</p>
申请公布号 EP2245421(A4) 申请公布日期 2013.07.10
申请号 EP20090713198 申请日期 2009.02.18
申请人 ADVANCED MATERIAL ENGINEERING PTE LTD 发明人 ANG, YONG LIM, THOMAS;NG, SAY HIM;AW, CHENG HOK
分类号 F42C15/42;F42C11/00;F42C11/06;F42C15/40;F42C17/00;F42C17/04;G01P3/66;G01P7/00 主分类号 F42C15/42
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