发明名称 CONTROL MOMENT GYROSCOPE
摘要 The objective of the present invention is to provide a control moment gyroscope which can be provided in a limited space since the volume thereof can be reduced without a change in performance by optimizing the shapes and mounting positions of each component. To this end, the control moment gyroscope of the present invention is a control moment gyroscope for generating torque in the orthogonal directions to both of two shafts which are perpendicularly disposed to each other by rotating the two shafts, and the control moment gyroscope comprises: a gimbal motor formed in the shape of a hollow cylinder and supplying momentum; spin motor provided in the inside of the gimbal motor and supplying momentum in a perpendicular direction to the momentum of the gimbal motor; and a flywheel provided in the inside of the gimbal motor and supplied with the rotational force of the gimbal motor and the rotational force of the spin motor.
申请公布号 EP2955114(A1) 申请公布日期 2015.12.16
申请号 EP20130879953 申请日期 2013.10.25
申请人 KOREA AEROSPACE RESEARCH INSTITUTE 发明人 LEE, SEON HO
分类号 B64G1/28;G01C19/04;G05D1/08 主分类号 B64G1/28
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