| 摘要 |
<p>PURPOSE:To improve shooting-down capability against an ultra high speed small-size target by a method wherein a guided missile is flown on the estimated flying track of the target into the same direction as the flying direction of the target and when a relative distance between the target entered within a predetermined distance, a propelling device is cut and separated to guide the missile toward the point of rendezvous independently. CONSTITUTION:Constituting components from an antenna 14 to a propelling device 24, which are attached substantially sequentially from the fore end in the propelling direction of a missile so far, are arranged in reverse excluding the propelling device and a guided missile M' is controlled so as to fly into the same direction as the flying direction of a target on the estimated track of the flying of the target by a commanding signal from a launcher during the initial and intermediate periods. An operating period deciding circuit 26 operates a relative distance between the target 1 by the output of an error signal generator 9 and when the distance has become within a predetermined relative distance, a high level signal is outputted. An auxiliary propelling device 29 accelerates a guided missile when the output of the operating period deciding circuit has become a high level signal and a propelling device separating machine 30 cuts and separates the auxiliary propelling device 29 and the propelling device 24 after the guided missile is accelerated.</p> |
