Design and performance of a Martian autonomous navigation system based on a smallsat constellation

dc.contributor.authorMolli, S.
dc.contributor.authorDurante, D.
dc.contributor.authorBoscagli, G.
dc.contributor.authorCascioli, Gael
dc.contributor.authorRacioppa, P.
dc.contributor.authorAlessi, E. M.
dc.contributor.authorSimonetti, S.
dc.contributor.authorVigna, L.
dc.contributor.authorIess, L.
dc.date.accessioned2023-01-19T20:48:08Z
dc.date.available2023-01-19T20:48:08Z
dc.date.issued2022-11-30
dc.description.abstractDeciphering the genesis and evolution of the Martian polar caps can provide crucial understanding of Mars’ climate system and will be a big step forward for comparative climatology of the terrestrial planets. The growing scientific interest for the exploration of Mars at high latitudes, together with the need of minimizing the resources onboard landers and rovers, motivates the need for an adequate navigation support from orbit. In the context of the ARES4SC study, we propose a novel concept based on a constellation that can support autonomous navigation of different kind of users devoted to scientific investigations of those regions. We study two constellations, that differ mainly for the semi-major axis and the inclination of the orbits, composed of 5 small satellites (based on the SmallSats design being developed in Argotec), offering dedicated coverage of the Mars polar regions. We focus on the architecture of the inter-satellite links (ISL), the key elements providing both ephemerides and time synchronization for the broadcasting of the navigation message. Our concept is based on suitably configured coherent links, able to suppress the adverse effects of on-board clock instabilities and to provide excellent range-rate accuracies between the constellation’s nodes. The data quality allows attaining good positioning performance for both constellations with a largely autonomous system. Indeed, we show that ground support can be heavily reduced by employing an ISL communication architecture. Periodic synchronization of the clocks on-board the constellation nodes with terrestrial time (TT) is enabled through the main spacecraft (the mother-craft), the only element of the constellation enabling radio communication with the Earth. We report on the results of numerical simulations in different operational scenarios and show that a very high-quality orbit reconstruction can be obtained for the constellation nodes using a batch-sequential filter or a batch filter with overlapping arcs, that could be implemented on board the mother-craft, thus enabling a high level of navigation autonomy. The assessment of the achievable positioning accuracy with this concept is fundamental to evaluate the feasibility of a future positioning system providing a global coverage of the red planet.en_US
dc.description.sponsorshipPart of this work was supported by a scientific agreement among University of Rome Sapienza, Italian National Research Council (CNR), and Argotec s. r.l. for a Ph.D. doctorate in aerospace engineering.en_US
dc.description.urihttps://www.sciencedirect.com/science/article/pii/S0094576522006488en_US
dc.format.extent13 pagesen_US
dc.genrejournal articlesen_US
dc.genrepreprintsen_US
dc.identifierdoi:10.13016/m2gqvu-3eo4
dc.identifier.citation"S. Molli et al. “Design and performance of a Martian autonomous navigation system based on a smallsat constellation.” Acta Astronautica 203 (February 2023): 112-124. https://doi.org/10.1016/j.actaastro.2022.11.041 "en_US
dc.identifier.urihttps://doi.org/10.1016/j.actaastro.2022.11.041
dc.identifier.urihttp://hdl.handle.net/11603/26691
dc.language.isoen_USen_US
dc.publisherElsevieren_US
dc.relation.isAvailableAtThe University of Maryland, Baltimore County (UMBC)
dc.relation.ispartofUMBC Center for Space Sciences and Technology
dc.relation.ispartofUMBC Faculty Collection
dc.rightsThis item is likely protected under Title 17 of the U.S. Copyright Law. Unless on a Creative Commons license, for uses protected by Copyright Law, contact the copyright holder or the author.en_US
dc.titleDesign and performance of a Martian autonomous navigation system based on a smallsat constellationen_US
dc.typeTexten_US
dcterms.creatorhttps://orcid.org/0000-0001-9070-7947en_US

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