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dc.contributor.authorHazry, Desa
dc.contributor.authorMohd Sofian, Muhamad Rosbi
dc.contributor.authorMuhamad Firdaus, Muhamad Dali
dc.date.accessioned2009-11-17T07:53:01Z
dc.date.available2009-11-17T07:53:01Z
dc.date.issued2009-10-11
dc.identifier.citationp.5A7 1 - 5A7 3en_US
dc.identifier.urihttp://dspace.unimap.edu.my/123456789/7311
dc.descriptionOrganized by School of Mechatronic Engineering (UniMAP) & co-organized by The Institution of Engineering Malaysia (IEM), 11th - 13th October 2009 at Batu Feringhi, Penang, Malaysia.en_US
dc.description.abstractThis paper is about study of control signal for Quadrotor UAV Flight Dynamics and Control strategies. Several observation and literature review have been done to evaluate and investigate the characteristic of control signal for Qundrotor UAV Radio Control (RC) technology is being chosen to be studied for determining the characteristic and behavior of control signal. RC control signal present about modulation of control signal with carrier signal with different technique and method of modulation which is Pulse Position Modulation (PPM), Pulse Code Modulation (PCM) and Pulse Width Modulation (PWM).en_US
dc.description.sponsorshipTechnical sponsored by IEEE Malaysia Sectionen_US
dc.language.isoenen_US
dc.publisherUniversiti Malaysia Perlisen_US
dc.relation.ispartofseriesProceedings of the International Conference on Man-Machine Systems (ICoMMS 2009)en_US
dc.subjectControl signalen_US
dc.subjectVehicles, Remotely piloteden_US
dc.subjectFlight controlen_US
dc.subjectGuidance systems (Flight)en_US
dc.subjectRadio controlen_US
dc.subjectAircraft -- Radio controlen_US
dc.titleStudy of control signal for Quadrotor UAVen_US
dc.typeWorking Paperen_US
dc.contributor.urlhazry@unimap.edu.myen_US


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