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Method of Conducting and Verification for Failure Mode Effect Test of Rotary Automatic Flight Control System Software

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dc.contributor.authorWooSung-Yeom-
dc.contributor.authorSeokwun-Ha-
dc.date.accessioned2024-12-02T21:30:52Z-
dc.date.available2024-12-02T21:30:52Z-
dc.date.issued2020-01-
dc.identifier.issn1225-1348-
dc.identifier.issn2287-6871-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/71892-
dc.description.abstractIt is necessary to develop digital flight control system by digital control technology to ensure stability and maneuverability of rotary helicopter. It is important to meet functional requirements of helicopter flight control system OFP and verify system reliability directly linked to flight safety as a core technology that avoids the transfer of technology by overseas advanced helicopter manufacturer. In this paper, we studied how to perform FMET for operational flight program of rotary automatic flight control system.-
dc.format.extent8-
dc.language한국어-
dc.language.isoKOR-
dc.publisher한국항공우주학회-
dc.titleMethod of Conducting and Verification for Failure Mode Effect Test of Rotary Automatic Flight Control System Software-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.doi10.5139/JKSAS.2020.48.1.55-
dc.identifier.scopusid2-s2.0-85118767998-
dc.identifier.wosid000537745700006-
dc.identifier.bibliographicCitationJournal of The Korean Society Aeronautical and Space Sciences, v.48, no.1, pp 55 - 62-
dc.citation.titleJournal of The Korean Society Aeronautical and Space Sciences-
dc.citation.volume48-
dc.citation.number1-
dc.citation.startPage55-
dc.citation.endPage62-
dc.type.docTypeArticle-
dc.identifier.kciidART002546537-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClassscopus-
dc.description.journalRegisteredClassesci-
dc.description.journalRegisteredClasskci-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryEngineering, Aerospace-
dc.subject.keywordAuthorAFCS-
dc.subject.keywordAuthorOFP-
dc.subject.keywordAuthorFMET-
dc.subject.keywordAuthorStability-
dc.subject.keywordAuthorReliability-
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공과대학 (항공우주및소프트웨어공학부)
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