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구동기 동역학의 영향을 고려한 BTT 미사일의 유도 조종 시스템 설계 : Design of an autopilotguidance system for BTT missiles considering actuator dynamics

DC Field Value Language
dc.contributor.advisor하인중-
dc.contributor.author홍진우-
dc.date.accessioned2010-02-02T16:09:32Z-
dc.date.available2010-02-02T16:09:32Z-
dc.date.copyright2007.-
dc.date.issued2007-
dc.identifier.urihttp://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000045161kog
dc.identifier.urihttps://hdl.handle.net/10371/48939-
dc.description學位論文(博士)--서울大學校 大學院 :電氣·컴퓨터工學部,2007.ko
dc.format.extentvii, 191장ko
dc.language.isokoko
dc.publisher서울大學校 大學院ko
dc.subject비행 체계ko
dc.subjectFlight Systemsko
dc.subjectBTT 미사일ko
dc.subjectBTT Missileko
dc.subject자동조종 제어기ko
dc.subjectAutopilot Controllerko
dc.subject최적 유도 법칙ko
dc.subjectOptimal Guidance Lawko
dc.subject핀 구동기 동역학ko
dc.subjectFin Actuator Dynamicsko
dc.subject자동조종장치 동역학ko
dc.subjectAutopilot Dynamicsko
dc.subject비최소위상 비선형 시스템ko
dc.subjectNonminimum-Phase Nonlinear Systemsko
dc.subject유사특이섭동기법ko
dc.subjectSingular Perturbation-like Techniqueko
dc.title구동기 동역학의 영향을 고려한 BTT 미사일의 유도 조종 시스템 설계ko
dc.title.alternativeDesign of an autopilotguidance system for BTT missiles considering actuator dynamicsko
dc.typeThesis-
dc.contributor.department電氣·컴퓨터工學部-
dc.description.degreeDoctorko
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