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충돌각을 고려한 BTT 미사일의 최적 종말 유도 법칙 설계 : Design of an Optimal Terminal Guidance Law for BTT Missiles Considering Impact Angles

DC Field Value Language
dc.contributor.advisor하인중-
dc.contributor.author조철-
dc.date.accessioned2010-01-29T06:11:23Z-
dc.date.available2010-01-29T06:11:23Z-
dc.date.copyright2009.-
dc.date.issued2009-
dc.identifier.urihttp://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000036043kog
dc.identifier.urihttps://hdl.handle.net/10371/46892-
dc.description학위논문(박사) --서울대학교 대학원 :전기. 컴퓨터공학부, 2009.2.ko
dc.format.extent143 p.ko
dc.language.isokoko
dc.publisher서울대학교 대학원ko
dc.subjectBTT 미사일ko
dc.subjectBTT missileko
dc.subject충돌각ko
dc.subjectimpact angleko
dc.subject최적 종말 유도 법칙ko
dc.subjectoptimal terminal guidance lawko
dc.subject자동조종장치 동역학ko
dc.subjectautopilot dynamicsko
dc.subject핀 구동기 동역학ko
dc.subjectfin actuator dynamicsko
dc.subject자동조종 제어기ko
dc.subjectautopilot controllerko
dc.subject유사특이섭동기법ko
dc.subjectsingular perturbation-like techniqueko
dc.subject비최소위상 비선형 시스템ko
dc.subjectnonminimum phase nonlinear systemko
dc.title충돌각을 고려한 BTT 미사일의 최적 종말 유도 법칙 설계ko
dc.title.alternativeDesign of an Optimal Terminal Guidance Law for BTT Missiles Considering Impact Anglesko
dc.typeThesis-
dc.contributor.department전기. 컴퓨터공학부-
dc.description.degreeDoctorko
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