Performance analysis of attitude-hold proportional navigation guidance for high-altitude defense missiles고고도 방어 유도탄의 자세유지 비례항법 성능 분석

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dc.contributor.advisorTahk, Min-Jea-
dc.contributor.advisor탁민제-
dc.contributor.authorYoon, SungJin-
dc.date.accessioned2021-05-11T19:34:48Z-
dc.date.available2021-05-11T19:34:48Z-
dc.date.issued2019-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=875549&flag=dissertationen_US
dc.identifier.urihttp://hdl.handle.net/10203/283123-
dc.description학위논문(석사) - 한국과학기술원 : 항공우주공학과, 2019.8,[v, 54 p. :]-
dc.description.abstractThe high - altitude defense missile is the precision guided munition responsible for the middle class of the missile defense system. A tilted seeker and Divert and Attitude Control System are applied to intercept the fast approaching ballistic missiles from high altitude to direct attack. In this paper, we propose a proportional navigation method to maintain the target in the FOV of the tilted seeker and takes into account the acceleration command of the DACS in the vertical direction of the KV’s body frame. Also, we compare the performance with the proportional navigation, analyze the performance of the proposed guidance law in various scenarios.-
dc.languageeng-
dc.publisher한국과학기술원-
dc.subjectHigh altitude defense missile▼atilted seeker▼aattitude hold▼akill vehicle▼anose cone-
dc.subject고고도 방어 미사일▼a편향된 탐색기▼a자세 유지▼a직격요격체▼a노즈콘-
dc.titlePerformance analysis of attitude-hold proportional navigation guidance for high-altitude defense missiles-
dc.title.alternative고고도 방어 유도탄의 자세유지 비례항법 성능 분석-
dc.typeThesis(Master)-
dc.identifier.CNRN325007-
dc.description.department한국과학기술원 :항공우주공학과,-
dc.contributor.alternativeauthor윤성진-
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AE-Theses_Master(석사논문)
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