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Adaptive Orbit Determination for Interplanetary Spacecraft

Show simple item record Burkhart, P. D. en_US Bishop, Robert H. en_US 2004-09-30T03:34:23Z 2004-09-30T03:34:23Z 1996 en_US
dc.identifier.citation Austin, Texas, USA en_US
dc.identifier.clearanceno 96-0363 en_US
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

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