Development of Nonlinear Flight Mechanical Model of High Aspect Ratio Light Utility Aircraft

dc.contributor.authorBahri, S.
dc.contributor.authorSasongko, R. A.
dc.date.accessioned2022-03-30T13:16:38Z
dc.date.available2022-03-30T13:16:38Z
dc.date.issued2018
dc.date.updated2022-03-27T13:35:22Z
dc.description.abstractThe implementation of Flight Control Law (FCL) for Aircraft Electronic Flight Control System (EFCS) aims to reduce pilot workload, while can also enhance the control performance during missions that require long endurance flight and high accuracy maneuver. In the development of FCL, a quantitative representation of the aircraft dynamics is needed for describing the aircraft dynamics characteristic and for becoming the basis of the FCL design. Hence, a 6 Degree of Freedom nonlinear model of a light utility aircraft dynamics, also called the nonlinear Flight Mechanical Model (FMM), is constructed. This paper shows the construction of FMM from mathematical formulation, the architecture design of FMM, the trimming process and simulations. The verification of FMM is done by analysis of aircraft behaviour in selected trimmed conditions.en
dc.identifier.eissn1742-6596
dc.identifier.issn1742-6588
dc.identifier.urihttps://depositonce.tu-berlin.de/handle/11303/16607
dc.identifier.urihttp://dx.doi.org/10.14279/depositonce-15384
dc.language.isoenen
dc.rights.urihttps://creativecommons.org/licenses/by/3.0/en
dc.subject.ddc530 Physikde
dc.subject.othernonlinear flight mechanical modelen
dc.subject.otherhigh aspect ratio light utility aircraften
dc.subject.otherFCLen
dc.subject.otherEFCSen
dc.subject.otherAircraft Electronic Flight Control Systemen
dc.titleDevelopment of Nonlinear Flight Mechanical Model of High Aspect Ratio Light Utility Aircraften
dc.typeArticleen
dc.type.versionpublishedVersionen
dcterms.bibliographicCitation.articlenumber012022en
dcterms.bibliographicCitation.doi10.1088/1742-6596/1005/1/012022en
dcterms.bibliographicCitation.issue1en
dcterms.bibliographicCitation.journaltitleJournal of Physics: Conference Seriesen
dcterms.bibliographicCitation.originalpublishernameIOPen
dcterms.bibliographicCitation.originalpublisherplaceBristolen
dcterms.bibliographicCitation.volume1005en
tub.accessrights.dnbfreeen
tub.affiliationFak. 5 Verkehrs- und Maschinensysteme::Inst. Luft- und Raumfahrtde
tub.affiliation.facultyFak. 5 Verkehrs- und Maschinensystemede
tub.affiliation.instituteInst. Luft- und Raumfahrtde
tub.publisher.universityorinstitutionTechnische Universität Berlinen

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