Incorporation of Orbital Dynamics to Improve Wide-Area Differential GPS

Ceva, J.; Bertinger, W.; Mullerschoen, R.; Yunck, T.; Parkinson, B.

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