Fl. Markley, ATTITUDE DETERMINATION USING VECTOR OBSERVATIONS - A FAST OPTIMAL MATRIX ALGORITHM, The Journal of the astronautical sciences, 41(2), 1993, pp. 261-280
The attitude matrix minimizing Wahba's loss function is computed direc
tly by a method that is either faster or more robust than any previous
ly known algorithm for finding this optimal estimate. Analysis of the
special case of two vector observations identifies those cases for whi
ch the TRIAD or algebraic method minimizes Wahba's loss function. The
new method also provides an estimate of the attitude error covariance
matrix, including an especially convenient representation of the two-o
bservation covariance matrix.