Publication Date:
2019-06-27
Description:
A comparison of three square root filter formulations with the standard extended Kalman filter is described. The characteristics of the algorithms were compared by simulating the application of a phase one GPS system to the determination of a LANDSAT-D Satellite.
Keywords:
ASTRODYNAMICS
Type:
NASA. Goddard Space Flight Center Flight Mech.(Estimation Theory Symp.; p 253-2279
Format:
application/pdf
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