A procedure to compute the integer ambiguity problem when a GPS receiver is used in a multiple antenna configuration attached to a rotating spacecraft is presented. The method is applied to a simulation of an experimental satellite which uses the GPS receiver for attitude determination.
Integer ambiguity resolution in GPS for spinning spacecrafts
IEEE Transactions on Aerospace and Electronic Systems ; 35 , 4 ; 1219-1229
1999-10-01
573736 byte
Article (Journal)
Electronic Resource
English
Integer ambiguity resolution in GPS for spinning spacecrafts
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