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Relative navigation system design for multiple spacecraft formation flying

DC Field Value Language
dc.contributor.advisor이장규-
dc.contributor.authorMuhammad Ilyas-
dc.date.accessioned2010-01-26T15:37:02Z-
dc.date.available2010-01-26T15:37:02Z-
dc.date.copyright2008.-
dc.date.issued2008-
dc.identifier.urihttp://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000042266eng
dc.identifier.urihttps://hdl.handle.net/10371/45023-
dc.descriptionThesis(masters) --서울대학교 대학원 :전기. 컴퓨터공학부,2008.8.en
dc.format.extentix, 117 p.en
dc.language.isoenen
dc.publisher서울대학교 대학원en
dc.subject상대적인 동적 모델en
dc.subjectRelative dynamic modelen
dc.subject편대 비행en
dc.subjectformation flyingen
dc.subject연합형 확장칼만필터en
dc.subjectfederated EKFen
dc.subject연합형 무편향 칼만 필터en
dc.subjectfederated UKFen
dc.subject고장 검출 및 분리en
dc.subjectFault Detection and Isolation (FDI)en
dc.titleRelative navigation system design for multiple spacecraft formation flyingen
dc.typeThesis-
dc.contributor.department전기. 컴퓨터공학부-
dc.description.degreeMasteren
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