TY - GEN
T1 - Orbit determination pipeline for geostationary objects using physics-informed neural networks
AU - Scorsoglio, Andrea
AU - D’Ambrosio, Andrea
AU - Campbell, Tanner
AU - Furfaro, Roberto
AU - Reddy, Vishnu
N1 - Publisher Copyright:
© 2024 by Andrea Scorsoglio, Andrea D'Ambrosio, Tanner Campbell, Roberto Furfaro, Vishnu Reddy.
PY - 2024
Y1 - 2024
N2 - Due to the importance of the geostationary orbit belt, tracking and identification of satellites in such orbits is of pivotal importance for space situational awareness. To address this problem, a comprehensive pipeline for satellite tracking is proposed, starting from raw observations to satellite identification and tracking. The pipeline includes "Stingray", an advanced hardware system with 15 cameras for high-resolution optical observations of the GEO belt. The astrometry component extracts the necessary information for orbit determination, while physics-informed neural networks (PINNs) estimate the object orbits, considering significant dynamics disturbances including third-body perturbations, solar radiation pressure and control maneuvers. The proposed framework is capable of processing the orbit determination of several objects in parallel and is able to automatically re-process all those observations for which the orbit determination previously failed by varying the PINN hyperparameters. Thus, the pipeline results to be accurate and efficient, thus being proper for catalog maintenance.
AB - Due to the importance of the geostationary orbit belt, tracking and identification of satellites in such orbits is of pivotal importance for space situational awareness. To address this problem, a comprehensive pipeline for satellite tracking is proposed, starting from raw observations to satellite identification and tracking. The pipeline includes "Stingray", an advanced hardware system with 15 cameras for high-resolution optical observations of the GEO belt. The astrometry component extracts the necessary information for orbit determination, while physics-informed neural networks (PINNs) estimate the object orbits, considering significant dynamics disturbances including third-body perturbations, solar radiation pressure and control maneuvers. The proposed framework is capable of processing the orbit determination of several objects in parallel and is able to automatically re-process all those observations for which the orbit determination previously failed by varying the PINN hyperparameters. Thus, the pipeline results to be accurate and efficient, thus being proper for catalog maintenance.
UR - http://www.scopus.com/inward/record.url?scp=85196769714&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85196769714&partnerID=8YFLogxK
U2 - 10.2514/6.2024-1862
DO - 10.2514/6.2024-1862
M3 - Conference contribution
AN - SCOPUS:85196769714
SN - 9781624107115
T3 - AIAA SciTech Forum and Exposition, 2024
BT - AIAA SciTech Forum and Exposition, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2024
Y2 - 8 January 2024 through 12 January 2024
ER -