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dc.contributor.authorHuang, L
dc.contributor.authorMurton, C
dc.date.accessioned2012-02-20T00:22:27Z
dc.date.available2012-02-20T00:22:27Z
dc.date.copyright2011-12
dc.date.issued2012-02-20
dc.identifier.citation15th International Conference on Mechatronic Technology 2011, 2011-11-30 - 2011-12-02, pages 12 - 16
dc.identifier.isbn978-0-7326-4018-7
dc.identifier.urihttp://hdl.handle.net/10292/3403
dc.description.abstractThis paper presents the development of a PCbased control system for an unmanned micro aerial vehicle (UAV) that has been converted from a helicopter model. The hand-controller of the helicopter model is modified to be a wireless link between a ground control computer (GCC) and the UAV, which carries sensors including an inertia measurement unit (IMU) and the actuators for the main rotor and pitch angle controls. A programming environment, written with the C# programming language, is set up for the implementation of control algorithms for the UAV. Manual and automatic modes of controlling the UAV are achieved. Implementation issues, such as the reliability of the IMU data for closed-loop control, are also discussed.
dc.publisherAUT University
dc.relation.urihttp://sites.google.com/site/2011icmt/downloadable-files
dc.rightsNOTICE: this is the author’s version of a work that was accepted for publication. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. Changes may have been made to this work since it was submitted for publication. A definitive version was subsequently published in (see Citation). The original publication is available at (see Publisher's Version)
dc.subjectControl
dc.subjectMicro Aerial Vehicle
dc.titleA control system for an unmanned micro aerial vehicle
dc.typeConference Contribution
dc.rights.accessrightsOpenAccess


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