Real-time onboard orbit propagator for planetary missionsOA
Real-time onboard orbit propagator for planetary missions
Tommaso Torrini;Antonio Genova;Simone Andolfo;Anna Maria Gargiulo;Pierluigi Federici;Riccardo Teodori;Martina Ciambellini
University of Rome"La Sapienza",Rome 00184,ItalyUniversity of Rome"La Sapienza",Rome 00184,ItalyUniversity of Rome"La Sapienza",Rome 00184,ItalyUniversity of Rome"La Sapienza",Rome 00184,ItalyUniversity of Rome"La Sapienza",Rome 00184,ItalyUniversity of Rome"La Sapienza",Rome 00184,ItalyUniversity of Rome"La Sapienza",Rome 00184,Italy
autonomous navigationhigh-fidelity orbit propagationnon-conservative force modelingonboard orbit determination
autonomous navigationhigh-fidelity orbit propagationnon-conservative force modelingonboard orbit determination
《航天动力学（英文）》 2026 (1)
25-51,27
The authors acknowledge the funding provided by Progetti Speciali Italiani S.r.l.,supported by the ASI grant n.2022-6-E.0,for the development of navigation software aimed at the autonomous navigation of microsatellites.Additionally,the ground-truth results presented in this work were derived using the GMAT software.
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