Model-based attitude estimation for multicopters

dc.contributor.authorBaránek, Radek
dc.contributor.authorŠolc, František
dc.date.accessioned2016-11-18T10:56:11Z
dc.date.available2016-11-18T10:56:11Z
dc.date.issued2014
dc.description.abstractThe paper deals with model-based attitude estimation for multicopters and is mainly focused on investigation of accuracy degradation due to wind and inaccurate model parameters which are conditions always present when using in real world. At first the need for model-base estimation is motivated. Then the multicopter model is described. Based on the mathematical model of multicopter, the estimation algorithm utilizing the extended Kalman filter is constructed. The main contribution of the paper is the investigation of the negative impact of the wind and of inaccurate knowledge of the model parameters.cs
dc.format.extent1535526 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.citationAdvances in electrical and electronic engineering. 2014, vol. 12, no. 5, p. 501-510 : ill.cs
dc.identifier.doi10.15598/aeee.v12i5.1151
dc.identifier.issn1336-1376
dc.identifier.issn1804-3119
dc.identifier.urihttp://hdl.handle.net/10084/116398
dc.language.isoencs
dc.publisherVysoká škola báňská - Technická univerzita Ostravacs
dc.relation.ispartofseriesAdvances in electrical and electronic engineeringcs
dc.relation.urihttp://dx.doi.org/10.15598/aeee.v12i5.1151cs
dc.rights© Vysoká škola báňská - Technická univerzita Ostrava
dc.rightsCreative Commons Attribution 3.0 Unported (CC BY 3.0)
dc.rights.accessopenAccess
dc.rights.urihttp://creativecommons.org/licenses/by/3.0/
dc.subjectattitude estimationcs
dc.subjectextended Kalman filtercs
dc.subjectmulticoptercs
dc.titleModel-based attitude estimation for multicopterscs
dc.typearticlecs
dc.type.statusPeer-reviewedcs
dc.type.versionpublishedVersioncs

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