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Method for controlling the spin axis attitude of a spinning spacecraft
Method for controlling the spin axis attitude of a spinning spacecraft
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机译:控制旋转航天器自旋轴姿态的方法
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摘要
A system located on board a geosynchronous satellite for detecting spin axis precession and developing thruster control signals for restoring the spin axis to the desired attitude. Fuel economy is enhanced by performing the major attitude correction at a time when the fuel expended contributes to that required for orbit inclination control.
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