JPL Technical Report Server

Incorporation of Orbital Dynamics to Improve Wide-Area Differential GPS

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dc.contributor.author Ceva, J. en_US
dc.contributor.author Bertinger, W. en_US
dc.contributor.author Mullerschoen, R. en_US
dc.contributor.author Yunck, T. en_US
dc.contributor.author Parkinson, B. en_US
dc.date.accessioned 2004-10-03T05:09:32Z
dc.date.available 2004-10-03T05:09:32Z
dc.date.issued 1995
dc.identifier.citation Institute of Navigation meeting on GPS technology en_US
dc.identifier.citation Palm Springs, CA en_US
dc.identifier.clearanceno 95-1125
dc.identifier.uri http://hdl.handle.net/2014/31443
dc.description.abstract A powerful technique to compute precise GPS satellite orbits for the FAA Wide-Area Augmentation System (WAAS) has been evaluated. This dynamical technique estimates GPS satellite states from a long history of measurements not only yields accurate orbit solutions, but it enables separation of orbit and satellite clock errors and yields orbit accuracies of better than one meter within the service volume, as compared to the JPL precise ephemerides. en_US
dc.format.extent 1821900 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Orbital dynamics GPS satellite Wide-Area Augmentation System WAAS orbit solutions ephemerides FAA navigation aid en_US
dc.title Incorporation of Orbital Dynamics to Improve Wide-Area Differential GPS en_US


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