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Integer ambiguity resolution in GPS for spinning spacecrafts

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3 Author(s)
C. Ferrando ; NahuelSat, Argentina ; A. Perez ; R. S. Sanchez Pena

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

Published in:

IEEE Transactions on Aerospace and Electronic Systems  (Volume:35 ,  Issue: 4 )