Attitude control of multicopter

dc.contributor.authorŠolc, František
dc.contributor.authorBaránek, Radek
dc.contributor.editorPihera, Josef
dc.contributor.editorSteiner, František
dc.date.accessioned2012-11-27T11:52:18Z
dc.date.available2012-11-27T11:52:18Z
dc.date.issued2012
dc.description.abstract-translatedThis article deals with the problem of attitude control of multicopters. At first the basic properties of multicopters are described. Regarding the attitude control, representation of attitude and computation of errors using rotation matrices are mentioned. Since the dynamics of rotation motion of multicopter around each axis is similar and almost independent to each other, the attitude control is split to three independent control loops. Then the construction of simplified model of multicopter with one degree of rotation freedom is described. Also the dynamics of thrusts of propellers are taken into account in the model. Finally one of the possible controller designs is described and for reference the results of controller with parameters tuned using MATLAB tool are shown.en
dc.format5 s.cs
dc.format.mimetypeapplication/pdf
dc.identifier.citationElectroscope. 2012, č. 5, EEICT 2012.cs
dc.identifier.issn1802-4564
dc.identifier.urihttp://hdl.handle.net/11025/712
dc.language.isoenen
dc.publisherZápadočeská univerzita v Plzni, Fakulta elektrotechnickács
dc.relation.ispartofseriesElectroscopecs
dc.rights© 2012 Electroscope. All rights reserved.en
dc.rights.accessopenAccessen
dc.subjectmultikoptéracs
dc.subjectřízení orientacecs
dc.subjectPID kontrolérycs
dc.subject.translatedmultricopteren
dc.subject.translatedattitude controlen
dc.subject.translatedPID controllersen
dc.titleAttitude control of multicopteren
dc.typečlánekcs
dc.typekonferenční příspěvekcs
dc.typearticleen
dc.typeconferenceObjecten
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen

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