Analysis of Attitude Errors in GRACE Range-Rate Residuals—A Comparison Between SCA1B and the Fused Attitude Product (SCA1B + ACC1B)

Publikation: Beitrag in FachzeitschriftArtikelForschungPeer-Review

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  • Technische Universität Graz
  • Max-Planck-Institut für Gravitationsphysik (Albert-Einstein-Institut)
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OriginalspracheEnglisch
Aufsatznummer5500604
FachzeitschriftIEEE Sensors Letters
Jahrgang2
Ausgabenummer2
Frühes Online-Datum12 Apr. 2018
PublikationsstatusVeröffentlicht - Juni 2018

Abstract

For missions such as GRACE, precise knowledge of the satellite's attitude is a fundamental requirement for the realization of the intersatellite ranging principle. It is not only essential for the realization of the precise in-orbit intersatellite pointing but also for the recovery of accurate temporal gravity field models. Here, we present a comparative study of two attitude datasets. One of them is the standard SCA1B RL02 datasets provided by JPL NASA, and another is a fused attitude dataset computed at TU Graz, based on the combination of ACC1B angular accelerations and SCA1B quaternions. Furthermore, we also present the impact of the attitude datasets on the intersatellite range measurements by analyzing their residuals. Our analysis reveals the significant improvement in the attitude due to the reprocessed product and reduced value of residuals computed from the reprocessed attitude.

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Analysis of Attitude Errors in GRACE Range-Rate Residuals—A Comparison Between SCA1B and the Fused Attitude Product (SCA1B + ACC1B). / Goswami, Sujata; Klinger, Beate; Weigelt, Matthias et al.
in: IEEE Sensors Letters, Jahrgang 2, Nr. 2, 5500604, 06.2018.

Publikation: Beitrag in FachzeitschriftArtikelForschungPeer-Review

Goswami S, Klinger B, Weigelt M, Mayer-Gürr T. Analysis of Attitude Errors in GRACE Range-Rate Residuals—A Comparison Between SCA1B and the Fused Attitude Product (SCA1B + ACC1B). IEEE Sensors Letters. 2018 Jun;2(2):5500604. Epub 2018 Apr 12. doi: 10.48550/arXiv.1802.02634, 10.1109/LSENS.2018.2825439
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title = "Analysis of Attitude Errors in GRACE Range-Rate Residuals—A Comparison Between SCA1B and the Fused Attitude Product (SCA1B + ACC1B)",
abstract = "For missions such as GRACE, precise knowledge of the satellite's attitude is a fundamental requirement for the realization of the intersatellite ranging principle. It is not only essential for the realization of the precise in-orbit intersatellite pointing but also for the recovery of accurate temporal gravity field models. Here, we present a comparative study of two attitude datasets. One of them is the standard SCA1B RL02 datasets provided by JPL NASA, and another is a fused attitude dataset computed at TU Graz, based on the combination of ACC1B angular accelerations and SCA1B quaternions. Furthermore, we also present the impact of the attitude datasets on the intersatellite range measurements by analyzing their residuals. Our analysis reveals the significant improvement in the attitude due to the reprocessed product and reduced value of residuals computed from the reprocessed attitude.",
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author = "Sujata Goswami and Beate Klinger and Matthias Weigelt and Torsten Mayer-G{\"u}rr",
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AU - Goswami, Sujata

AU - Klinger, Beate

AU - Weigelt, Matthias

AU - Mayer-Gürr, Torsten

N1 - ACKNOWLEDGMENT The authors would like to thank the DFG Sonderforschungsbereich SFB 1128 Relativistic Geodesy and Gravimetry with Quantum Sensors (geo-Q) for financial support. The authors would also like to thank Prof. J. Flury for providing the space and resources to work.

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AB - For missions such as GRACE, precise knowledge of the satellite's attitude is a fundamental requirement for the realization of the intersatellite ranging principle. It is not only essential for the realization of the precise in-orbit intersatellite pointing but also for the recovery of accurate temporal gravity field models. Here, we present a comparative study of two attitude datasets. One of them is the standard SCA1B RL02 datasets provided by JPL NASA, and another is a fused attitude dataset computed at TU Graz, based on the combination of ACC1B angular accelerations and SCA1B quaternions. Furthermore, we also present the impact of the attitude datasets on the intersatellite range measurements by analyzing their residuals. Our analysis reveals the significant improvement in the attitude due to the reprocessed product and reduced value of residuals computed from the reprocessed attitude.

KW - attitude errors

KW - GRACE

KW - range-rate residuals

KW - sensor fusion

KW - Sensor systems

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