Please use this identifier to cite or link to this item: http://cmuir.cmu.ac.th/jspui/handle/6653943832/54480
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dc.contributor.authorMana Saedanen_US
dc.contributor.authorPinyo Puangmalien_US
dc.date.accessioned2018-09-04T10:14:28Z-
dc.date.available2018-09-04T10:14:28Z-
dc.date.issued2015-09-08en_US
dc.identifier.other2-s2.0-84957615573en_US
dc.identifier.other10.1109/ASCC.2015.7244561en_US
dc.identifier.urihttps://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84957615573&origin=inwarden_US
dc.identifier.urihttp://cmuir.cmu.ac.th/jspui/handle/6653943832/54480-
dc.description.abstract© 2015 IEEE. Electric motor and propeller selection is an important key in designing a radio controlled aircraft especially when designing a new type of aircraft. Since the characteristics of commercial RC electric motors and propellers are usually not reported, this paper hence demonstrates experiments to determine suitable pairs of motors and propellers that produces enough forces for an aircraft within constraints. The developed test bed utilized simple load cells to determine lifting forces and drag moments of propellers is presented. The investigated characteristics of motor/propeller including averaged lifting forces, averaged drag moments, maximum temperature of motors, and also input electrical current and power are reported.en_US
dc.subjectEngineeringen_US
dc.titleCharacterization of motor and propeller sets for a small radio controlled aircraften_US
dc.typeConference Proceedingen_US
article.title.sourcetitle2015 10th Asian Control Conference: Emerging Control Techniques for a Sustainable World, ASCC 2015en_US
article.stream.affiliationsChiang Mai Universityen_US
Appears in Collections:CMUL: Journal Articles

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