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위성발사체의 궤적최적화와 관성유도 알고리듬 설계에 관한 연구 : A Study on the trajectory optimization and inertial guidance algorithm design for satellite launch vehicles

DC Field Value Language
dc.contributor.advisor김유단-
dc.contributor.author노웅래-
dc.date.accessioned2010-01-15T05:57:51Z-
dc.date.available2010-01-15T05:57:51Z-
dc.date.copyright2001.-
dc.date.issued2001-
dc.identifier.urihttp://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000066357kor
dc.identifier.urihttps://hdl.handle.net/10371/31721-
dc.description학위논문(박사)--서울대학교 대학원 :항공우주공학과,2001.ko
dc.format.extentxiv, 175 p.ko
dc.language.isokoko
dc.publisher서울대학교 대학원ko
dc.subjectatellite launch vehicleko
dc.subject위성발사체ko
dc.subjecttrajectory optimizationko
dc.subject궤적최적화ko
dc.subjecttime finite element methodko
dc.subject시간유한요소법ko
dc.subjectdirect collocationko
dc.subject준상태변수추정ko
dc.subjectcostate estimationko
dc.subject관성유도ko
dc.title위성발사체의 궤적최적화와 관성유도 알고리듬 설계에 관한 연구ko
dc.title.alternativeA Study on the trajectory optimization and inertial guidance algorithm design for satellite launch vehiclesko
dc.typeThesis-
dc.contributor.department항공우주공학과-
dc.description.degreeDoctorko
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