Impact of Deployable Solar Panels on Gravity Field Recovery in GRACE-like Satellites

a Closed-Loop Simulation Study

verfasst von: Andreas Leipner, Alexey Kupriyanov, Arthur Reis, Annike Knabe, Manuel Schilling, Vitali Müller, Matthias Weigelt, Jürgen Müller, Meike List
Abstract: Future satellite gravimetry missions must meet increasing scientific demands, requiring advanced technologies, e.g., novel inertial sensors, laser ranging systems and potentially electric thrusters to operate in a drag-free regime. Deployable solar panels offer a promising solution by providing sufficient power even under unfavorable illumination conditions, without significantly increasing satellite dimensions or mass. This study evaluates the impact of single and double deployable solar panels on gravity field recovery (GFR) through closed-loop simulations. Five GRACE-like satellite configurations were analyzed, each with distinct finite element models and inertia properties. Detailed orbit simulations included non-spherical static gravity field and impacting non-gravitational force models. Satellites drag coefficients varied from 2.25 to 4.5, depending on configuration. GFR was assessed using degree RMS of spherical harmonic coefficient differences between the recovered and reference fields. GFR results show that discrepancies between the modified and standard configurations are mainly driven by variations of the actuation noise of the modeled optical accelerometer - simplified gravitational reference sensor (SGRS). SGRS performance, in turn, depends on the satellite’s cross-sectional area. Moreover, the convergence of residuals in the spectral domain for simulated orbits with different drag coefficients confirmed the dominant role of SGRS performance in the retrieved gravity field.
Organisationseinheit(en): Institut für Erdmessung
Externe Organisation(en): Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)
Max-Planck-Institut für Gravitationsphysik (Albert-Einstein-Institut)
Typ: Artikel
Journal: Journal of Geodesy
Band: 99
ISSN: 0949-7714
Publikationsdatum: 04.07.2025
Publikationsstatus: Veröffentlicht
Peer-reviewed: Ja
ASJC Scopus Sachgebiete: Geophysik, Geochemie und Petrologie, Computer in den Geowissenschaften
Elektronische Version(en): https://doi.org/10.1007/s00190-025-01983-1 (Zugang: Offen)
https://doi.org/10.48550/ARXIV.2503.21651 (Zugang: Offen)
: Details im Forschungsportal „Research@Leibniz University“

BibTeX

@article{ba00b63fd3884f62b37ecaa2e4574b7a,
title = "Impact of Deployable Solar Panels on Gravity Field Recovery in GRACE-like Satellites: a Closed-Loop Simulation Study",
abstract = "Future satellite gravimetry missions must meet increasing scientific demands, requiring advanced technologies, e.g., novel inertial sensors, laser ranging systems and potentially electric thrusters to operate in a drag-free regime. Deployable solar panels offer a promising solution by providing sufficient power even under unfavorable illumination conditions, without significantly increasing satellite dimensions or mass. This study evaluates the impact of single and double deployable solar panels on gravity field recovery (GFR) through closed-loop simulations. Five GRACE-like satellite configurations were analyzed, each with distinct finite element models and inertia properties. Detailed orbit simulations included non-spherical static gravity field and impacting non-gravitational force models. Satellites drag coefficients varied from 2.25 to 4.5, depending on configuration. GFR was assessed using degree RMS of spherical harmonic coefficient differences between the recovered and reference fields. GFR results show that discrepancies between the modified and standard configurations are mainly driven by variations of the actuation noise of the modeled optical accelerometer - simplified gravitational reference sensor (SGRS). SGRS performance, in turn, depends on the satellite{\textquoteright}s cross-sectional area. Moreover, the convergence of residuals in the spectral domain for simulated orbits with different drag coefficients confirmed the dominant role of SGRS performance in the retrieved gravity field.",
keywords = "Closed-loop simulation, Finite element modeling, Future satellite gravimetry missions, Gravity field recovery, Optical accelerometry, Satellite shapes",
author = "Andreas Leipner and Alexey Kupriyanov and Arthur Reis and Annike Knabe and Manuel Schilling and Vitali M{\"u}ller and Matthias Weigelt and J{\"u}rgen M{\"u}ller and Meike List",
note = "Publisher Copyright: {\textcopyright} The Author(s) 2025.",
year = "2025",
month = jul,
day = "4",
doi = "10.1007/s00190-025-01983-1",
language = "English",
volume = "99",
journal = "Journal of Geodesy",
issn = "0949-7714",
publisher = "Springer Verlag",
number = "7",
}