发明名称 GUIDED MISSILE
摘要 <p>PURPOSE:To improve a follow-up performance against a super-high speed small- sized target. CONSTITUTION:Composing elements of the prior art device are arranged in their opposite direction except a propulsion device 24, and further there are provided an operation period discriminating circuit 26 for use in discriminating in response to a relative distance for the prior art device, an accelerating and propulsion auxiliary propulsion device 29, a propulsion device separating mechanism 30 for separating the propulsion device or the like, a propulsion device separation sensing circuit 31 for use in sensing the separation, a missile alignment delay circuit 32 for sensing an alignment of the missile and outputting a control signal and an operation starting instruction circuit 33 for instructing a starting of function for use in locking-on on a target 1. A relative speed with respect to the target is controlled to cause a timing for triggering the missile explosive to be better and then a performance for shooting down the target is improved.</p>
申请公布号 JPH04297796(A) 申请公布日期 1992.10.21
申请号 JP19910044990 申请日期 1991.03.11
申请人 MITSUBISHI ELECTRIC CORP 发明人 SAITO OSAMU
分类号 B64C13/20;F41G7/22;F42B15/01;F42B15/36;F42C11/00;F42C13/04;G01S13/88;G05D1/12 主分类号 B64C13/20
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