发明名称 MOMENT CONTROL UNIT FOR SPACECRAFT ATTITUDE CONTROL
摘要 <p>A moment control device (120) for positioning a spacecraft which employs a plurality of spinning bodies (122, 124, 126, 128) operable to impart a desired torque to a space craft, the bodies being constructed in a unitary combination and the unitary combination being mounted to the spacecraft to be positioned.</p>
申请公布号 WO2000012269(A2) 申请公布日期 2000.03.09
申请号 US1999017764 申请日期 1999.08.05
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