Generalized missile guidance law for impact angle control일반화된 충돌각 제어 유도법칙 연구

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dc.contributor.advisorTahk, Min-Jea-
dc.contributor.advisor탁민제-
dc.contributor.authorLee, Yong-In-
dc.contributor.author이용인-
dc.date.accessioned2013-09-11-
dc.date.available2013-09-11-
dc.date.issued2012-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=487163&flag=dissertation-
dc.identifier.urihttp://hdl.handle.net/10203/179632-
dc.description학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2012.2, [ vii, 128 p. ]-
dc.languageeng -
dc.publisher한국과학기술원-
dc.subjectimpact angle control-
dc.subjectguidance law-
dc.subjectoptimality-
dc.subjectanalytic solution-
dc.subject유도법칙-
dc.subject충돌각 제어-
dc.subject최적성-
dc.subject해석해-
dc.subject시스템 지연-
dc.subjectsystem lag-
dc.titleGeneralized missile guidance law for impact angle control-
dc.title.alternative일반화된 충돌각 제어 유도법칙 연구-
dc.typeThesis(Ph.D)-
dc.identifier.CNRN487163/325007 -
dc.description.department한국과학기술원 : 항공우주공학전공, -
dc.identifier.uid020085308-
dc.contributor.localauthorTahk, Min-Jea-
dc.contributor.localauthor탁민제-
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AE-Theses_Ph.D.(박사논문)
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