基本信息:
- 专利标题： 제어 모멘트 자이로스코프 및 이를 포함하는 소형 인공위성
- 专利标题（英）：Control moment gyroscope and cube type satellite including the same
- 申请号：KR1020170039871 申请日：2017-03-29
- 公开(公告)号：KR101796541B1 公开(公告)日：2017-12-01
- 发明人： 김홍래 , 권성철 , 박기연 , 이성환 , 박재필
- 申请人： (주)나라스페이스테크놀로지
- 申请人地址： 서울특별시 종로구 숭인동길 ** ,***동****호(숭인동,종로청계힐스테이트)
- 专利权人： (주)나라스페이스테크놀로지
- 当前专利权人： (주)나라스페이스테크놀로지
- 当前专利权人地址： 서울특별시 종로구 숭인동길 ** ,***동****호(숭인동,종로청계힐스테이트)
- 代理人： 김재형
- 主分类号： G01C19/08
- IPC分类号： G01C19/08 ; G08C17/02 ; G01S19/01
The present invention relates to relates to a control moment gyroscope, enabling the precise position control of the small artificial satellite and that can improve the posture control mobility control moment gyroscope.
More specifically, the present invention is a control moment gyroscope for controlling the attitude of flight body, the mounting being fixed to the navigation unit body; It is disposed above the mounting portion, and the upper rotating part being the center rotatably connected to the first rotation axis relative to said mounting portion; Flywheel contained in said upper rotating part, which is rotatably connected to the second rotation axis is perpendicular to the first axis of rotation and; And a second drive motor for rotating and driving the flywheel; It relates to a control moment gyroscope comprising: a; the second driving power required for driving the motor the wireless power supply system for supplying wireless power transmission unit as.