Towards the 1-cm SARAL orbit
Autor: | Xu Yang, Brian D. Beckley, D. E. Pavlis, Jesse Wimert, Frank G. Lemoine, Nikita P. Zelensky, O. Bordyugov, Douglas S. Chinn |
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Rok vydání: | 2016 |
Předmět: |
Atmospheric Science
010504 meteorology & atmospheric sciences Spacecraft business.industry Coordinate system Satellite laser ranging Aerospace Engineering DORIS (geodesy) Astronomy and Astrophysics 01 natural sciences Geophysics Amplitude Space and Planetary Science 0103 physical sciences Orbit (dynamics) General Earth and Planetary Sciences Satellite Altimeter business 010303 astronomy & astrophysics 0105 earth and related environmental sciences Remote sensing Mathematics |
Zdroj: | Advances in Space Research. 58:2651-2676 |
ISSN: | 0273-1177 |
DOI: | 10.1016/j.asr.2015.12.011 |
Popis: | We have investigated the quality of precise orbits for the SARAL altimeter satellite using Satellite Laser Ranging (SLR) and Doppler Orbitography and Radiopositioning Integrated by Satellite (DORIS) data from March 14, 2013 to August 10, 2014. We have identified a 4.31 ± 0.14 cm error in the Z (cross-track) direction that defines the center-of-mass of the SARAL satellite in the spacecraft coordinate system, and we have tuned the SLR and DORIS tracking point offsets. After these changes, we reduce the average RMS of the SLR residuals for seven-day arcs from 1.85 to 1.38 cm. We tuned the non-conservative force model for SARAL, reducing the amplitude of the daily adjusted empirical accelerations by eight percent. We find that the best dynamic orbits show altimeter crossover residuals of 5.524 cm over cycles 7–15. Our analysis offers a unique illustration that high-elevation SLR residuals will not necessarily provide an accurate estimate of radial error at the 1-cm level, and that other supporting orbit tests are necessary for a better estimate. Through the application of improved models for handling time-variable gravity, the use of reduced-dynamic orbits, and through an arc-by-arc estimation of the C22 and S22 coefficients, we find from analysis of independent SLR residuals and other tests that we achieve 1.1–1.2 cm radial orbit accuracies for SARAL. The limiting errors stem from the inadequacy of the DPOD2008 and SLRF2008 station complements, and inadequacies in radiation force modeling, especially with respect to spacecraft self-shadowing and modeling of thermal variations due to eclipses. |
Databáze: | OpenAIRE |
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