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소형 항공기 조종면 고장검출 알고리즘 연구

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dc.contributor.author이호영-
dc.contributor.author전남주-
dc.contributor.author함형진-
dc.contributor.author이형철-
dc.date.accessioned2024-12-20T06:30:12Z-
dc.date.available2024-12-20T06:30:12Z-
dc.date.issued2013-10-
dc.identifier.urihttps://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/202990-
dc.description.abstractThis paper presents a fault diagnosis algorithm of an aileron of a small aircraft through analyzing the vibration signal of an accelerometer and RPM signal and using ANPSD, PCA and dual threshold method. The flight test of a actual aircraft was performed to construct a normal state database and to verify this algorithm. As a result, the possibility to apply this algorithm to an actual aircraft could be confirmed.-
dc.format.extent4-
dc.language한국어-
dc.language.isoKOR-
dc.publisher항공우주시스템공학회-
dc.title소형 항공기 조종면 고장검출 알고리즘 연구-
dc.title.alternativeStudy for a Fault Detection Algorithm of a Small Aircraft Aileron-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.bibliographicCitation항공우주시스템공학회 2013년도 추계학술대회, pp 1 - 4-
dc.citation.title항공우주시스템공학회 2013년도 추계학술대회-
dc.citation.startPage1-
dc.citation.endPage4-
dc.type.docTypeProceeding-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClassother-
dc.subject.keywordAuthorAileron Fault(조종면 고장)-
dc.subject.keywordAuthorFault Detection(고장검출)-
dc.subject.keywordAuthorPrincipal Component Analysis(주성분 분석)-
dc.subject.keywordAuthorDual Threshold(이중 임계값)-
dc.identifier.urlhttps://sase.or.kr/publication/publication03_list.asp-
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서울 공과대학 > 서울 전기공학전공 > 1. Journal Articles

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