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New approach to resolving instantaneous integer ambiguity resolution for spacecraft attitude determination using GPS signals

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2 Author(s)
Hodgart, M.S. ; Surrey Univ., Guildford, UK ; Purivigraipong, S.

A fast 3-part method is introduced for the solution of the attitude of a low Earth orbit satellite using the GPS system as a source of phase information. A possibly novel method is used to overcome the well known integer ambiguity problem, involving the Gram Schmidt orthogonalization procedure at one stage and a fast replacement for the usual QUEST solution of the least mean square attitude solution

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Position Location and Navigation Symposium, IEEE 2000

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