NASA NTRS · 20210004930
Adaptive Orbit Determination for Interplanetary Spacecraft
Abstract
The interplanetary orbit problem has been traditionally solved using least-squares techniques. Due to operational limitations of this method, a Kalman filter approach has been proposed for future missions which includes all spacecraft and measurement modeling states in the filter.
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Bishop, Robert H., Burkhart, P. D.. 1996-01-01. Adaptive Orbit Determination for Interplanetary Spacecraft. https://ntrs.nasa.gov/citations/20210004930
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