发明名称 CHASING AND DECOYING SIMULATION APPARATUS BETWEEN AIRCRAFT WITH FLARE AND SEEKER AND METHOD THEREOF
摘要 The present invention provides a flare-based chasing and decoying simulation device between an aircraft and a seeker, capable of verifying interaction performance between an aircraft, a flare, and an infrared seeker by simulating whether the infrared seeker of a guided missile is decoyed using the flare. According to the present invention, the flare-based chasing and decoying simulation device includes: a simulation aircraft representing the aircraft operated in accordance with a simulation scenario and including a first IR lamp indicating a flare property of an actual exhaust port of the aircraft; a simulation flare including a second IR lamp indicating the property of the flare which the aircraft launches; an IR seeker recognizing one among the simulation flare and the simulation aircraft as a target based on a light property of the first and second IR lamps in accordance with a predetermined determination method; and a lamp control unit controlling an illumination intensity of the first and second IR lamps by estimating a generated amount of infrared rays of the flare and the flare in the exhaust port of the aircraft viewed from the seeker in accordance with an approaching rate of the seeker, a combustion property, a trace of the flare and the aircraft in accordance with the simulation scenario.
申请公布号 KR20160049321(A) 申请公布日期 2016.05.09
申请号 KR20140146288 申请日期 2014.10.27
申请人 AGENCY FOR DEFENSE DEVELOPMENT 发明人 SHIN, DONG CHO;CHOE, WON SEOK
分类号 B64F5/00;B64D45/00;F41H11/02 主分类号 B64F5/00
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