Device, system and method for attitude control

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United States of America Patent

PATENT NO 9850009
SERIAL NO

14651632

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Abstract

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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.

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Patent Owner(s)

Patent OwnerAddress
ISRAEL AEROSPACE INDUSTRIES LTD7010000 LOD

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Verbin, Dov Harrarit, IL 1 5

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