发明名称 Device, system and method for attitude control
摘要 A control moment gyroscope (CMG) is provided, selectively having a first spatial configuration and a second spatial configuration at least during operation of the CMG. In the first spatial configuration the CMG occupies a smaller volume than in the second spatial configuration. For example, in the first spatial configuration no part of the CMG projects beyond a predetermined geometrical boundary, while in the second spatial configuration, a portion of the CMG projects beyond the geometrical boundary.
申请公布号 IL223899(D0) 申请公布日期 2013.06.27
申请号 IL20120223899 申请日期 2012.12.26
申请人 ISRAEL AEROSPACE INDUSTRIES LTD.;VERBIN DOV 发明人
分类号 B64G 主分类号 B64G
代理机构 代理人
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