Aspects Regarding Fly Control of Quadcopter

A tétel rövid nézete
dc.creatorKuantama, Endrowednes
dc.creatorTarca, Ioan
dc.creatorTarca, Radu
dc.creatorCraciun, Dan
dc.date2016-09-14
dc.date.accessioned2020-09-11T08:33:51Z
dc.date.available2020-09-11T08:33:51Z
dc.descriptionQuadcopter 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.
dc.formatapplication/pdf
dc.identifierhttps://ojs.lib.unideb.hu/rIim/article/view/3854
dc.identifier10.17667/riim.2016.1-2/7.
dc.identifier.urihttp://hdl.handle.net/2437/295760
dc.languageeng
dc.publisherDebreceni Egyetem
dc.relationhttps://ojs.lib.unideb.hu/rIim/article/view/3854/3731
dc.sourceRecent Innovations in Mechatronics; Vol. 3 No. 1-2. (2016); 1-5.
dc.sourceRecent Innovations in Mechatronics; Évf. 3 szám 1-2. (2016); 1-5.
dc.source2064-9622
dc.subjectquadcopter
dc.subjectattitude
dc.subjectgyroscope
dc.subjectfly control
dc.subjectorientation sensor
dc.titleAspects Regarding Fly Control of Quadcopter
dc.typeinfo:eu-repo/semantics/article
dc.typeinfo:eu-repo/semantics/publishedVersion
dc.typePeer-reviewed Article
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Recent Innovations in Mechatronics (OJS)