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IN-FLIGHT TARGET IMPACT ANGLE DETERMINATION APPARATUS FOR BIASED PROPORTIONAL NAVIGATION GUIDANCE, METHOD THEREOF, AND COMPUTER READABLE STORAGE MEDIUM HAVING METHOD
IN-FLIGHT TARGET IMPACT ANGLE DETERMINATION APPARATUS FOR BIASED PROPORTIONAL NAVIGATION GUIDANCE, METHOD THEREOF, AND COMPUTER READABLE STORAGE MEDIUM HAVING METHOD
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机译：偏置比例导航制导的机上目标撞击角确定装置，方法及其计算机可读存储介质的确定方法
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摘要
The present invention relates to a flight vehicle navigation technique and, more specifically, relates to an in-flight target impact angle determination apparatus for biased proportional navigation guidance and a method thereof. According to the present invention, an in-flight target impact angle generated by relative geometry changed in launching time and hitting time.;COPYRIGHT KIPO 2018
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