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Implementation of a Multiplicative Extended Kalman Filter (MEKF) for Spinning Spacecraft Attitude Determination in the Astrodynamics Environment (ADE)
By: Kenneth J. Ernandes, Benjamin E. Joseph and Paul J. Cefola.
Pub. 2007, 11pgs.
PDF File. AAS 07-337.
Price: $29.00
 

Reprinted from Advances in the Astronautical Sciences Volume 129.

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