Adaptive Orbit Determination for Interplanetary Spacecraft

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

dc.contributor.author	Burkhart, P. D.	en_US
dc.contributor.author	Bishop, Robert H.	en_US
dc.date.accessioned	2004-09-30T03:34:23Z
dc.date.available	2004-09-30T03:34:23Z
dc.date.issued	1996	en_US
dc.identifier.citation	Austin, Texas, USA	en_US
dc.identifier.clearanceno	96-0363	en_US
dc.identifier.uri	http://hdl.handle.net/2014/24335
dc.description.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.	en_US
dc.format.extent	441242 bytes
dc.format.mimetype	application/pdf
dc.language.iso	en_US
dc.subject.other	adaptive Kalman filtering modeling least-squares Kalman filte	en_US
dc.title	Adaptive Orbit Determination for Interplanetary Spacecraft	en_US