Combined optical line-of-sight and crosslink radiometric navigation for distributed deep-space systems

Journal Article (2023)
Author(s)

S. Casini (TU Delft - Space Systems Egineering)

E. Turan (TU Delft - Space Systems Egineering)

A Cervone (TU Delft - Astrodynamics & Space Missions)

Bert Monna (Phosphoenix)

Pieter Visser (TU Delft - Space Engineering)

Research Group
Space Systems Egineering
Copyright
© 2023 S. Casini, E. Turan, A. Cervone, Bert Monna, P.N.A.M. Visser
DOI related publication
https://doi.org/10.1038/s41598-023-43339-9
More Info
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Publication Year
2023
Language
English
Copyright
© 2023 S. Casini, E. Turan, A. Cervone, Bert Monna, P.N.A.M. Visser
Research Group
Space Systems Egineering
Issue number
1
Volume number
13
Pages (from-to)
16253
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Abstract

This manuscript aims to present and evaluate the applicability of combining optical line-of-sight (LoS) navigation with crosslink radiometric navigation for deep-space cruising distributed space systems. To do so, a set of four distributed space systems architectures is presented, and for each of those, the applicability of the combination is evaluated, comparing it to the baseline solutions, which are based on only optical navigation. The comparison is done by studying the performance in a circular heliocentric orbit in seven different time intervals (ranging from 2024 to 2032) and exploiting the observation of all the pairs of planets from Mercury to Saturn. The distance between spacecraft is kept around 200 km. Later, a NEA mission test case is generated in order to explore the applicability to a more realistic case. This analysis shows that the technique can also cope with a variable inter-satellite distance, and the best performance is obtained when the spacecraft get closer to each other.