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FlightGear application for flight simulation of a mini-UAV

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dc.title FlightGear application for flight simulation of a mini-UAV en
dc.contributor.author Vogeltanz, Tomáš
dc.contributor.author Jašek, Roman
dc.relation.ispartof Proceedings of the International Conference of Numerical Analysis and Applied Mathematics 2014 (ICNAAM-2014)
dc.identifier.issn 0094-243X Scopus Sources, Sherpa/RoMEO, JCR
dc.identifier.isbn 978-0-7354-1287-3
dc.date.issued 2015
utb.relation.volume 1648
dc.event.title International Conference on Numerical Analysis and Applied Mathematics (ICNAAM)
dc.event.location Rhodes
utb.event.state-en Greece
utb.event.state-cs Řecko
dc.event.sdate 2014-09-22
dc.event.edate 2014-09-28
dc.type conferenceObject
dc.language.iso en
dc.publisher American Institute of Physics (AIP)
dc.identifier.doi 10.1063/1.4912769
dc.relation.uri http://scitation.aip.org/content/aip/proceeding/aipcp/10.1063/1.4912769
dc.subject aircraft en
dc.subject airplane en
dc.subject autopilot en
dc.subject FlightGear en
dc.subject modelling en
dc.subject PID en
dc.subject simulation en
dc.subject UAV en
dc.description.abstract This paper presents using of FlightGear application for flight simulation of a mini-UAV (Unmanned Aerial Vehicle). The first part of the paper is about general information of UAVs and about the fundamentals of airplane flight mechanics. The main section summarizes the information about FlightGear application and describes a way of using the application to simulate a mini-UAV. The process of altitude change by using autopilot has been simulated. In the created simulation, three stage cascade controller was used for an altitude control. Heading was controlled by 2 stage cascade PID (Proportional-Integral-Derivative) controller. An automatic throttle system was applied for a velocity control. The setting of all controllers is included in the description of the simulation. Finally, the results of FlightGear simulation are discussed. en
utb.faculty Faculty of Applied Informatics
dc.identifier.uri http://hdl.handle.net/10563/1005220
utb.identifier.obdid 43871611
utb.identifier.scopus 2-s2.0-84939648404
utb.identifier.wok 000355339703045
utb.source d-wok
dc.date.accessioned 2015-07-15T08:42:23Z
dc.date.available 2015-07-15T08:42:23Z
dc.rights Attribution-NonCommercial-NoDerivs 3.0 Unported
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/3.0/
dc.rights.access openAccess
utb.contributor.internalauthor Vogeltanz, Tomáš
utb.contributor.internalauthor Jašek, Roman
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