Momentum Space Analysis for Mixed Skew Angle Arrays

This report explores non-redundant constant-speed single-gimballed control moment gyroscope mechanics for spacecraft maneuvers. A 3/4 control moment gyroscope pyramid design was examined. This report focuses on maximum available momentum for mixed skew angle configurations. A method to maximize off-...

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Bibliographic Details
Main Author: Lewis, Zachary A.
Format: Book Chapter
Language:English
Published: IntechOpen 2020
Subjects:
Online Access:https://www.intechopen.com/chapters/67815
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