Aspects Regarding Fly Control of Quadcopter

A tétel rövid nézete
dc.contributor.authorEndrowednes, Kuantama
dc.contributor.authorIoan, Tarca
dc.contributor.authorRadu, Tarca
dc.contributor.authorDan, Craciun
dc.date.accessioned2016-09-14T09:24:18Z
dc.date.available2016-09-14T09:24:18Z
dc.date.issued2016-09-14
dc.description.abstractQuadcopter is one of Unmanned Aerial Vehicle (UAV) which has two pairs of identical fixed pitched rotor propellers. It can fly autonomously based on pre-programmed flight or manually controlled by a remote, and every movement achieved by varying the speed of each rotor independently. The orientation of quadcopter axes relative to a reference line and its direction of motion are known as attitude. Fly control factors are affected by attitude determination which can be calculated from 3 possible angles using combined measurement. Gyroscope and accelerometer are primary sensors to control quadcopter attitude, but magnetometer sensor and GPS also used to enhance the stability during flight. This paper will focus on details of function and mathematical formula of every factor regarding fly control and comparative data of 2 types of orientation sensor used in this system.hu_HU
dc.identifier.doi10.17667/riim.2016.1-2/7.hu_HU
dc.identifier.issn2064-9622hu_HU
dc.identifier.issue1-2hu_HU
dc.identifier.urihttp://hdl.handle.net/2437/230424
dc.identifier.volume3hu_HU
dc.language.isoenhu_HU
dc.publisherDUPresshu_HU
dc.publisher.placeDebrecenhu_HU
dc.rightsNevezd meg! - Ne add el! - Ne változtasd! 2.5 Magyarország*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/2.5/hu/*
dc.subjectquadcopterhu_HU
dc.subjectattitudehu_HU
dc.subjectgyroscopehu_HU
dc.subjectfly controlhu_HU
dc.subjectorientation sensorhu_HU
dc.titleAspects Regarding Fly Control of Quadcopterhu_HU
dc.typeArticlehu_HU
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Recent Innovations in Mechatronics