A device and method for improving spacecraft attitude stability
A stability and spacecraft technology, applied in attitude control and other directions, can solve problems such as torque gyro vibration spacecraft
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[0065] A six-degree-of-freedom decoupling vibration isolation method for a single-frame control moment gyroscope can be completed through the following steps:
[0066] A device for improving the attitude stability of a spacecraft, named as a vibration isolation element; the vibration isolation element includes an inner sleeve 1 and an outer sleeve 2; the inner sleeve 1 and the outer sleeve 2 are hollow cylinders with top ends; The diameter of the cross-section of the sleeve 1 is smaller than the diameter of the cross-section of the outer sleeve 2; the inner sleeve 1 is placed in the outer sleeve 2, and there is a gap between the inner sleeve 1 and the outer sleeve 2, and the metal spring 3 is placed in the gap, and the metal spring 3 is placed in the gap. The number of springs 3 is five, of which one metal spring 3 is located in the gap at the top, and the other four are evenly distributed in the gaps of the cylinder wall; the inner sleeve 1 of the vibration isolation element i...
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