DocumentCode
2989177
Title
Deriving a unique reference frame for GPS measurements
Author
Malla, Rajendra P. ; Wu, Sien-Chong
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
1988
fDate
29 Nov-2 Dec 1988
Firstpage
177
Lastpage
184
Abstract
Two strategies for deriving a unique reference frame for GPS (Global Positioning System) measurements are discussed. The first strategy utilizes the precise relative positions which have been predetermined by VLBI (very long baseline interferometry) to fix the frame orientation and the absolute scaling, while the offset from geocenter is determined from GPS measurements. Three different cases are presented under this strategy. The second strategy establishes a reference frame by holding only the longitudinal of one of the tracking sites fixed. The absolute scaling is determined by the adopted gravitational constant (GM) of the Earth; and the latitude is inferred from the time signature of the Earth´s rotation in the GPS measurements. The coordinate system thus defined will be a geocentric Earth fixed coordinate system. A covariance analysis shows that geometric positioning to an accuracy of a few centimeters can be achieved with just one day of precise GPS pseudorange and carrier phase data
Keywords
geodesy; radionavigation; radiowave interferometry; GPS measurements; Global Positioning System; VLBI; adopted gravitational constant; carrier phase data; covariance analysis; geometric positioning; latitude; precise GPS pseudorange; time signature; unique reference frame; very long baseline interferometry; Coordinate measuring machines; Earth; Equations; Extraterrestrial measurements; Global Positioning System; Moon; Motion measurement; Performance analysis; Poles and zeros; Satellite ground stations;
fLanguage
English
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium, 1988. Record. Navigation into the 21st Century. IEEE PLANS '88., IEEE
Conference_Location
Orlando, FL
Type
conf
DOI
10.1109/PLANS.1988.195481
Filename
195481
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