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Real-time onboard orbit propagator for planetary missions

Tommaso Torrini Antonio Genova Simone Andolfo Anna Maria Gargiulo Pierluigi Federici Riccardo Teodori Martina Ciambellini

航天动力学（英文）2026，Vol.10Issue(1)：25-51,27.

航天动力学（英文）2026，Vol.10Issue(1)：25-51,27.DOI:10.1007/s42064-025-0264-6

Real-time onboard orbit propagator for planetary missions

Tommaso Torrini ¹Antonio Genova ¹Simone Andolfo ¹Anna Maria Gargiulo ¹Pierluigi Federici ¹Riccardo Teodori ¹Martina Ciambellini¹

作者信息

1. University of Rome"La Sapienza",Rome 00184,Italy
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摘要

关键词

autonomous navigation/high-fidelity orbit propagation/non-conservative force modeling/onboard orbit determination

Key words

autonomous navigation/high-fidelity orbit propagation/non-conservative force modeling/onboard orbit determination

引用本文复制引用

Tommaso Torrini,Antonio Genova,Simone Andolfo,Anna Maria Gargiulo,Pierluigi Federici,Riccardo Teodori,Martina Ciambellini..Real-time onboard orbit propagator for planetary missions[J].航天动力学（英文）,2026,10(1):25-51,27.

基金项目

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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