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NASA NTRS · 20210004930

Adaptive Orbit Determination for Interplanetary Spacecraft

Bishop, Robert H.·Burkhart, P. D.
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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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BibTeXRIS

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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