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
1996-01-01
Miscellaneous
No indication
English
Adaptive Orbit Determination for Interplanetary Spacecraft
Online Contents | 1996
|Adaptive Orbit Determination for Interplanetary Spacecraft
British Library Conference Proceedings | 1996
|