发明名称 CONTROL DEVICE, AIRCRAFT, MISSILE GUIDANCE TAKEOVER PROGRAM, AND MISSILE GUIDANCE TAKEOVER METHOD
摘要 PROBLEM TO BE SOLVED: To prevent a missile from being useless even when an aircraft having fired the missile completes guidance of the missile.SOLUTION: A control device 20 loaded on an aircraft 10 capable of guiding a missile 14 having been fired transmits a guiding aircraft change instruction to be information for changing the aircraft guiding the missile 14 having been fired by the own aircraft to an accompanying aircraft, receives a guidance starting report to be information indicating starting of guidance of the missile 14 having been fired by the own aircraft from the accompanying aircraft to which the guiding aircraft change instruction is transmitted, and when receiving the guidance starting report, completes guidance of the missile 14 having been fired by the own aircraft.
申请公布号 JP2014074573(A) 申请公布日期 2014.04.24
申请号 JP20120223483 申请日期 2012.10.05
申请人 MITSUBISHI HEAVY IND LTD 发明人 YAMAMOTO TOSHITAKA
分类号 F41G7/30;G01S13/88 主分类号 F41G7/30
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