Routine operational and high-precision orbit determination of envisat
Autor: | P. L. Righetti, Michiel Otten, René Zandbergen, D. Kuijper, J.M. Dow |
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Rok vydání: | 2003 |
Předmět: |
Atmospheric Science
Spacecraft Computer science business.industry Aerospace Engineering DORIS (geodesy) Astronomy and Astrophysics Earth observation satellite Software package law.invention Geophysics Space and Planetary Science Radar altimeter law General Earth and Planetary Sciences Tracking data Orbit (control theory) business Orbit determination Remote sensing |
Zdroj: | Advances in Space Research. 31:1953-1958 |
ISSN: | 0273-1177 |
Popis: | ESA's Earth observation satellite Envisat was successfully launched on 1 March 2002 by an Ariane-5 launcher, and ESOC immediately took over the task of determining and predicting the orbit using S-band tracking data, and optimising the manoeuvre sequence to bring the spacecraft into an orbit accurately phased with ERS-2. On-board, Envisat carries, among others, a radar altimeter, a DORIS instrument and a laser retro-reflector array (SLR). Data from these instruments are being used at ESOC for high-precision orbit determination, for verification of the routine orbit determination and for cross-comparison with orbits computed on-board by the DORIS navigator and with those delivered with the Envisat products. This paper presents the first consolidated results obtained for Envisat routine and high-precision orbit determination. All orbit determination and control activities were performed with the software package NAPEOS, which was developed in-house. |
Databáze: | OpenAIRE |
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