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Adaptive Orbit Determination for Interplanetary Spacecraft

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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


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