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1000 Titel
  • Sentinel-6A precise orbit determination using a combined GPS/Galileo receiver
1000 Autor/in
  1. Montenbruck, Oliver |
  2. Hackel, Stefan |
  3. Wermuth, Martin |
  4. Zangerl, Franz |
1000 Erscheinungsjahr 2021
1000 Publikationstyp
  1. Artikel |
1000 Online veröffentlicht
  • 2021-09-05
1000 Erschienen in
1000 Quellenangabe
  • 95(9):109
1000 Copyrightjahr
  • 2021
1000 Lizenz
1000 Verlagsversion
  • https://doi.org/10.1007/s00190-021-01563-z |
1000 Publikationsstatus
1000 Begutachtungsstatus
1000 Sprache der Publikation
1000 Abstract/Summary
  • <jats:title>Abstract</jats:title><jats:p>The Sentinel-6 (or Jason-CS) altimetry mission provides a long-term extension of the Topex and Jason-1/2/3 missions for ocean surface topography monitoring. Analysis of altimeter data relies on highly-accurate knowledge of the orbital position and requires radial RMS orbit errors of less than 1.5 cm. For precise orbit determination (POD), the Sentinel-6A spacecraft is equipped with a dual-constellation GNSS receiver. We present the results of Sentinel-6A POD solutions for the first 6 months since launch and demonstrate a 1-cm consistency of ambiguity-fixed GPS-only and Galileo-only solutions with the dual-constellation product. A similar performance (1.3 cm 3D RMS) is achieved in the comparison of kinematic and reduced-dynamic orbits. While Galileo measurements exhibit 30–50% smaller RMS errors than those of GPS, the POD benefits most from the availability of an increased number of satellites in the combined dual-frequency solution. Considering obvious uncertainties in the pre-mission calibration of the GNSS receiver antenna, an independent inflight calibration of the phase centers for GPS and Galileo signal frequencies is required. As such, Galileo observations cannot provide independent scale information and the estimated orbital height is ultimately driven by the employed forces models and knowledge of the center-of-mass location within the spacecraft. Using satellite laser ranging (SLR) from selected high-performance stations, a better than 1 cm RMS consistency of SLR normal points with the GNSS-based orbits is obtained, which further improves to 6 mm RMS when adjusting site-specific corrections to station positions and ranging biases. For the radial orbit component, a bias of less than 1 mm is found from the SLR analysis relative to the mean height of 13 high-performance SLR stations. Overall, the reduced-dynamic orbit determination based on GPS and Galileo tracking is considered to readily meet the altimetry-related Sentinel-6 mission needs for RMS height errors of less than 1.5 cm.</jats:p>
1000 Sacherschließung
lokal Original Article
lokal Galileo
lokal SLR
lokal Jason-CS
lokal Precise orbit determination
lokal Sentinel-6
lokal Altimetry
lokal Single-receiver ambiguity fixing
lokal GPS
1000 Liste der Beteiligten
  1. https://orcid.org/0000-0003-4783-745X|https://orcid.org/0000-0002-8014-7146|https://frl.publisso.de/adhoc/uri/V2VybXV0aCwgTWFydGlu|https://frl.publisso.de/adhoc/uri/WmFuZ2VybCwgRnJhbno=
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  • DeepGreen-ID: 14a1899915c84c57b8ea52841e359fc2 ; metadata provieded by: DeepGreen (https://www.oa-deepgreen.de/api/v1/), LIVIVO search scope life sciences (http://z3950.zbmed.de:6210/livivo), Crossref Unified Resource API (https://api.crossref.org/swagger-ui/index.html), to.science.api (https://frl.publisso.de/), ZDB JSON-API (beta) (https://zeitschriftendatenbank.de/api/), lobid - Dateninfrastruktur für Bibliotheken (https://lobid.org/resources/search)
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1000 Erstellt am 2023-05-11T14:56:18.014+0200
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1000 Zuletzt bearbeitet 2023-10-24T08:17:46.521+0200
1000 Objekt bearb. Tue Oct 24 08:17:46 CEST 2023
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