태양위치추적 캔위성의 설계 및 제작 Design of Solar Tracking CanSat

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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.
Publisher
한국항공우주학회
Issue Date
2012-11-15
Language
Korean
Citation

2012 한국항공우주학회 추계학술대회, pp.926 - 929

URI
http://hdl.handle.net/10203/227029
Appears in Collection
RIMS Conference Papers
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