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Method and apparatus for rate integration supplement for attitude referencing with quaternion differencingA control system for providing attitude control in spacecraft. The control system comprising a primary attitude reference system, a secondary attitude reference system, and a hyper-complex number differencing system. The hyper-complex number differencing system is connectable to the primary attitude reference system and the secondary attitude reference system.
Document ID
20080004972
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - Patent
Authors
Rodden, John James
Price, Xenophon
Carrou, Stephane
Stevens, Homer Darling
Date Acquired
August 24, 2013
Publication Date
September 24, 2002
Subject Category
Astrodynamics
Report/Patent Number
Patent Number: US-PATENT-6,454,217
Patent Application Number: US-PATENT-APPL-SN-670904
Funding Number(s)
CONTRACT_GRANT: NAS7-1260
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-6,454,217
Patent Application
US-PATENT-APPL-SN-670904

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