Romeshkani, Mohsen und Müller, Jürgen und Ebadi, Sahar und Knabe, Annike und Schilling, Manuel (2026) Accelerometer Data Transplant for Future Satellite Gravimetry. Earth and Space Science, 13 (1), e2025EA004417. American Geophysical Union (AGU). doi: 10.1029/2025EA004417. ISSN 2333-5084.
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Offizielle URL: https://dx.doi.org/10.1029/2025EA004417
Kurzfassung
Accurate monitoring of the Earth's gravity field is crucial for understanding mass redistribution processes related to climate change, hydrology, and geodynamics. The Gravity Recovery and Climate Experiment (GRACE) and its successor, GRACE Follow-On (GRACE-FO), have provided invaluable satellite gravimetry data through low-low satellite-to-satellite tracking (LL-SST). However, the precision of gravity field recovery is significantly affected not only by data gaps in the accelerometer (ACC) measurements, but also by potential failures or limitations in their performance. To mitigate these issues, accelerometer data transplantation has been employed, leveraging the similarity in non-gravitational accelerations experienced by both satellites. This study presents an in-depth assessment of transplant noise and evaluates advanced accelerometer configurations, including Cold Atom Interferometry (CAI) accelerometers and hybrid electrostatic-quantum accelerometer setups for future satellite gravimetry missions. Through closed-loop LL-SST simulations, we compare four different accelerometer configurations, ranging from conventional electrostatic accelerometers (EAs) to fully hybrid CAI-EA setups. Results indicate that a dual hybrid accelerometer configuration offers the highest accuracy in gravity field recovery, while a transplant-based hybrid approach significantly enhances the performance of non-gravitational force modeling without requiring additional instrumentation. The findings underscore the potential of quantum accelerometery and transplant methodologies for future satellite gravimetry missions, offering a cost-effective solution to improve gravity field recovery, while benefitting from new sensor types.
| elib-URL des Eintrags: | https://elib.dlr.de/221688/ | ||||||||||||||||||||||||
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| Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||
| Titel: | Accelerometer Data Transplant for Future Satellite Gravimetry | ||||||||||||||||||||||||
| Autoren: |
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| Datum: | 2026 | ||||||||||||||||||||||||
| Erschienen in: | Earth and Space Science | ||||||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||||||
| Open Access: | Ja | ||||||||||||||||||||||||
| Gold Open Access: | Ja | ||||||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||||||
| In ISI Web of Science: | Ja | ||||||||||||||||||||||||
| Band: | 13 | ||||||||||||||||||||||||
| DOI: | 10.1029/2025EA004417 | ||||||||||||||||||||||||
| Seitenbereich: | e2025EA004417 | ||||||||||||||||||||||||
| Verlag: | American Geophysical Union (AGU) | ||||||||||||||||||||||||
| ISSN: | 2333-5084 | ||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||
| Stichwörter: | Accelerometer, data transplant, satellite gravimetry, quantum sensor | ||||||||||||||||||||||||
| 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 - Missionsstudie CARIOQA [KNQ], R - Inertial Sensing for Space Applications | ||||||||||||||||||||||||
| Standort: | Hannover | ||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Satellitengeodäsie und Inertialsensorik > Satellitengeodäsie und geodätische Modellierung | ||||||||||||||||||||||||
| Hinterlegt von: | Schilling, Manuel | ||||||||||||||||||||||||
| Hinterlegt am: | 06 Jan 2026 12:16 | ||||||||||||||||||||||||
| Letzte Änderung: | 06 Jan 2026 12:16 |
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