Adaptive Orbit Determination for Interplanetary Spacecraft

Burkhart, P. D.; Bishop, Robert H.

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Adaptive Orbit Determination for Interplanetary Spacecraft

Burkhart, P. D.; Bishop, Robert H.

URI: http://hdl.handle.net/2014/24335

Date: 1996

Citation: Austin, Texas, USA

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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