DC Field | Value | Language |
---|---|---|
dc.contributor.author | 정인지 | ko |
dc.contributor.author | 문지환 | ko |
dc.contributor.author | 김민수 | ko |
dc.date.accessioned | 2017-11-20T08:21:14Z | - |
dc.date.available | 2017-11-20T08:21:14Z | - |
dc.date.created | 2017-11-13 | - |
dc.date.issued | 2012-11-15 | - |
dc.identifier.citation | 2012 한국항공우주학회 추계학술대회, pp.926 - 929 | - |
dc.identifier.uri | http://hdl.handle.net/10203/227029 | - |
dc.description.abstract | In 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.language | Korean | - |
dc.publisher | 한국항공우주학회 | - |
dc.title | 태양위치추적 캔위성의 설계 및 제작 | - |
dc.title.alternative | Design of Solar Tracking CanSat | - |
dc.type | Conference | - |
dc.type.rims | CONF | - |
dc.citation.beginningpage | 926 | - |
dc.citation.endingpage | 929 | - |
dc.citation.publicationname | 2012 한국항공우주학회 추계학술대회 | - |
dc.identifier.conferencecountry | KO | - |
dc.identifier.conferencelocation | 라마다프라자제주호텔 | - |
dc.contributor.nonIdAuthor | 문지환 | - |
dc.contributor.nonIdAuthor | 김민수 | - |
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