NASA NTRS · 20080004972
Method and apparatus for rate integration supplement for attitude referencing with quaternion differencing
Abstract
A 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.
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Rodden, John James, Price, Xenophon, Carrou, Stephane, Stevens, Homer Darling. 2002-09-24. Method and apparatus for rate integration supplement for attitude referencing with quaternion differencing. https://ntrs.nasa.gov/citations/20080004972
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