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Leveraging Spire CubeSats and ICGEM Models for Improved Gravity Field Solutions

Shafiei, Parisa und Weigelt, Matthias und Tabibi, Sajad (2025) Leveraging Spire CubeSats and ICGEM Models for Improved Gravity Field Solutions. IAG Scientific Assembly, 2025-09-01 - 2025-09-05, Rimini, Italien.

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Kurzfassung

In 2016, Spire Global Inc. began manufacturing commercial CubeSats to analyze Radio Occultation (RO) data from Global Navigation Satellite Systems (GNSS). While RO measurements have been used for various applications, including atmospheric research and ice sheet height estimation, the zenith-looking Precise Orbit Determination (POD) antenna introduces new possibilities for geodetic applications. Each Spire LEMUR CubeSat is equipped with a dual-frequency Global Positioning System (GPS) antenna and an Attitude Determination and Control System (ADCS). Leveraging the measurements provided by the POD antenna and the ADCS, Earth’s gravity field recovery emerges as a promising application, offering new opportunities for the geoscience community . The POD of Spire CubeSats constellation, performed using the raw observation approach, has been applied to model Earth’s gravity field through the short arc method. The Spire CubeSats, with different orbital characteristics, can be used individually or in combination to analyze the time-variable components of the Earth’s gravity field. However, cCombining individual gravity field solutions results in improved accuracy compared to standalone models. This framework provides the opportunity of combining Spire-based gravity field models with those obtained from low Earth orbit (LEO) dedicated or non-dedicated gravimetric missions that offer higher accuracy. In this contribution, monthly gravity field solutions from 10 Spire CubeSats constellation are combined with the ICGEM monthly solutions at the normal equations level (NEQs) using the variance component estimation (VCE). The quality of the combined Spire + SST-hl + SLR monthly gravity field solutions is then compared with the ITSG-GRACE gravity field model for 2020.

elib-URL des Eintrags:https://elib.dlr.de/221676/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Leveraging Spire CubeSats and ICGEM Models for Improved Gravity Field Solutions
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Shafiei, Parisaparisa.shafiei (at) uni.luNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Weigelt, Matthiasmatthias.weigelt (at) dlr.dehttps://orcid.org/0000-0001-9669-127XNICHT SPEZIFIZIERT
Tabibi, Sajadsajad.tabibi (at) uni.luNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:4 September 2025
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Spire CubeSat GNSS POD Gravity Field Recovery Satellite Gravimetry Short-arc approach
Veranstaltungstitel:IAG Scientific Assembly
Veranstaltungsort:Rimini, Italien
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:1 September 2025
Veranstaltungsende:5 September 2025
Veranstalter :IAG
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Kommunikation, Navigation, Quantentechnologien
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R KNQ - Kommunikation, Navigation, Quantentechnologie
DLR - Teilgebiet (Projekt, Vorhaben):R - Inertial Sensing for Space Applications
Standort: Hannover
Institute & Einrichtungen:Institut für Satellitengeodäsie und Inertialsensorik > Satellitengeodäsie und geodätische Modellierung
Hinterlegt von: Weigelt, Matthias
Hinterlegt am:30 Dez 2025 15:39
Letzte Änderung:15 Jan 2026 10:07

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