태양위치추적 캔위성의 설계 및 제작Design of Solar Tracking CanSat

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dc.contributor.author정인지ko
dc.contributor.author문지환ko
dc.contributor.author김민수ko
dc.date.accessioned2017-11-20T08:21:14Z-
dc.date.available2017-11-20T08:21:14Z-
dc.date.created2017-11-13-
dc.date.issued2012-11-15-
dc.identifier.citation2012 한국항공우주학회 추계학술대회, pp.926 - 929-
dc.identifier.urihttp://hdl.handle.net/10203/227029-
dc.description.abstractIn this paper the design and fabrication process of a CanSat which can trace the sun as well as send GPS and attitude information. IMU and servo motors used to conrol its attitude. In order that the solar sensor of the CanSat in always directed to the sun. A passive low pass filter used to reduce the noisy output of the sensor. That results show that attitude control of the CanSat and its solar sensor in successful.-
dc.languageKorean-
dc.publisher한국항공우주학회-
dc.title태양위치추적 캔위성의 설계 및 제작-
dc.title.alternativeDesign of Solar Tracking CanSat-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.beginningpage926-
dc.citation.endingpage929-
dc.citation.publicationname2012 한국항공우주학회 추계학술대회-
dc.identifier.conferencecountryKO-
dc.identifier.conferencelocation라마다프라자제주호텔-
dc.contributor.nonIdAuthor문지환-
dc.contributor.nonIdAuthor김민수-
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