Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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Development of A CanSat System Applying High Agility Camera and Remote Control Camera

고기동 안정화 카메라 및 원격제어 셀프카메라를 적용한 캔위성 시스템 개발

  • Kim, Su-Hyeon (Department of Aerospace Engineering, Chosun University) ;
  • Park, Jae-Hyeon (Department of Aerospace Engineering, Chosun University) ;
  • Kim, Hye-In (Department of Aerospace Engineering, Chosun University) ;
  • Bea, Gi-Sung (Department of Aerospace Engineering, Chosun University) ;
  • Chae, Bong-Geon (Dream Space World) ;
  • Oh, Hyun-Ung (Department of Aerospace Engineering, Chosun University)
  • 김수현 (조선대학교 항공우주공학과) ;
  • 박재현 (조선대학교 항공우주공학과) ;
  • 김혜인 (조선대학교 항공우주공학과) ;
  • 배기성 (조선대학교 항공우주공학과) ;
  • 채봉건 (드림스페이스월드) ;
  • 오현웅 (조선대학교 항공우주공학과)
  • Received : 2018.05.16
  • Accepted : 2018.06.14
  • Published : 2018.06.30
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Abstract

The High Agility and Remote Control Camera System Can-Satellite ($HA+RC^2S$ CanSat) proposed in this study is a satellite designed by the authors of this work and submitted as an entry in the 2017 CanSat competition in Goheung gun, Jeonnam, Korea. The primary mission of this work is to develop a high agility camera system (HACS) that can obtain high quality images in the air. This objective is achieved by using a tuned mass damper (TMD) to attenuate the residual vibration that occurs immediately after rotating the camera. The secondary objective is to obtain a self-image of CanSat in the air using a remote control self-camera system (RCSS) that is wirelessly controlled using a joystick from a ground station. This paper describes the development process of the $HA+RC^2S$ CanSat, including mission definition, system design, manufacturing, function and performance tests carried out on the ground, and final launch test.

본 논문에서 제안한 캔위성은 2017년 캔위성 경연대회에 출전한 $HA+RC^2S$ CanSat (High Agility and Remote Control Camera System Can Satellite)이다. 주요임무는 수동진동감쇠기인 동흡진기를 사용하여 카메라를 회전시킨 직후에 발생하는 잔류진동을 감쇠하여 고품질의 영상획득이 가능한 고기동 안정화 카메라 시스템을 검증하는 것이다. 부가적으로는 지상국의 조이스틱을 사용하여 무선으로 제어되는 원격 제어 셀프카메라로 캔위성 자체의 이미지데이터를 획득하는 것이다. 본 논문에서는 임무 정의, 시스템 설계, 제작, 기능 및 성능시험, 최종 비행시험을 포함하는 $HA+RC^2S$ CanSat의 개발과정에 대해 서술하였다.

Keywords

References

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