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.
Adaptive Orbit Determination for Interplanetary Spacecraft
01.01.1996
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Englisch
Adaptive Orbit Determination for Interplanetary Spacecraft
Online Contents | 1996
|Adaptive Orbit Determination for Interplanetary Spacecraft
British Library Conference Proceedings | 1996
|