Spacecraft Attitude Determination Using Global Positioning Satellite Signals
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(17)
With
(18)
For which
is the iteration number and
. This
equation can be solved for
using Gaussian elimination or decomposition methods. The algorithms described in this paper use Gaussian elimination methods (Gauss-Newton-Levenberg-Marquardt Method).
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(17)
(18)
. This 
using Gaussian elimination or decomposition methods. The algorithms described in this paper use Gaussian elimination methods (Gauss-Newton-Levenberg-Marquardt Method).