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Please use this identifier to cite or link to this item: http://uyr.uy.edu.mm/handle/123456789/148
dc.contributor.authorPa Pa Winn San
dc.contributor.authorZaw Min Aung
dc.contributor.authorChaw Myat Nwe
dc.contributor.authorZaw Min Naing
dc.date.accessioned2016-11-07T20:08:35Z
dc.date.available2016-11-07T20:08:35Z
dc.date.issued2010
dc.identifier.urihttp://uyr.uy.edu.mm/handle/123456789/148
dc.descriptionProceedings of the Second International Conference on Science and Engineering organized by Ministry of Science and Technology on December 2-3, 2010 at Sedona hotel, Yangon, Myanmar
dc.description.abstractThe purpose of doing this research is to develop and implement altitude control system for holding of aerial vehicle. This paper emphasizes on the longitudinal stability control system. Experimental autonomous flight vehicle developed by Tamkang University is used as the application airframe as it gives coefficients to get the very accurate model of aircraft flight behaviour. An altitude hold control structure is constructed classical designs. The structure contains two control loops. The inner loop is for altitude rate regulation. In this control loop, the combination of altitude rate and pitch angle are used as the feedback signals. The simulation results of the inner loop are used to design the outer altitude control loop. The inner control loop for this research work is considered in this paper.
dc.subjectautonomous flight vehicle system
dc.subjectaltitude holding system
dc.subjectelevator control
dc.subjectlongitudinal stability
dc.subjectbode plot
dc.titleDevelopment of Altitude Control System for Autonomous Flight Vehiclelanguage
dc.typeconferenceObject


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