Geographically correlated errors observed from a laser-based short-arc technique

Citation
P. Bonnefond et al., Geographically correlated errors observed from a laser-based short-arc technique, J GEO RES-O, 104(C7), 1999, pp. 15885-15893
Citations number
16
Categorie Soggetti
Earth Sciences
Journal title
JOURNAL OF GEOPHYSICAL RESEARCH-OCEANS
ISSN journal
21699275 → ACNP
Volume
104
Issue
C7
Year of publication
1999
Pages
15885 - 15893
Database
ISI
SICI code
0148-0227(19990715)104:C7<15885:GCEOFA>2.0.ZU;2-T
Abstract
The laser-based short-are technique has been developed in order to avoid lo cal errors which affect the dynamical orbit computation, such as those due to mismodeling in the geopotential. It is based on a geometric method and c onsists in fitting short arcs (about 4000 km), issued from a global orbit, with satellite laser ranging tracking measurements from a ground station ne twork. Ninety-two TOPEX/Poseidon (T/P) cycles of laser-based short-are orbi ts have then been compared to JGM-2 and JGM-3 T/P orbits computed by the Pr ecise Orbit Determination (POD) teams (Service d'Orbitographie Doris/Centre National d'Etudes Spatiales and Goddard Space Plight Center/NASA) over two areas: (1) the Mediterranean area and (2) a part of the Pacific (including California and Hawaii) called hereafter the U.S. area. Geographically corr elated orbit errors in these areas are clearly evidenced: for example, -2.6 cm and +0.7 cm for the Mediterranean and U.S. areas, respectively, relativ e to JGM3 orbits. However, geographically correlated errors (GCE) which are commonly linked to errors in the gravity model, can also be due to systema tic errors in the reference frame and/or to biases in the tracking measurem ents. The short-are technique being very sensitive to such error sources, o ur analysis however demonstrates that the induced geographical systematic e ffects are at the level of 1-2 cm on the radial orbit component. Results ar e also compared with those obtained with the GPS-based reduced dynamic tech nique. The time-dependent part of GCE has also been studied. Over 6 years o f T/P data, coherent signals in the radial component of T/P Precise Orbit E phemeris (POE) are clearly evidenced with a time period of about 6 months. In addition, impact of time varying-error sources coming from the reference frame and the tracking data accuracy has been analyzed, showing a possible linear trend of about 0.5-1 mm/yr in the radial component of T/P POE.