Deciphering the genesis and evolution of the Martian polar caps can provide critical understanding of Mars’ climate system and allow us to apply the lesson learned on the Earth about planetary climate change on other terrestrial planets. In this work, we present a novel mission concept that can support autonomous navigation of rovers devoted to scientific investigations of these regions. We propose a constellation of 5 small satellites with coverage over Mars polar regions, focusing on the positioning performance that can be obtained. Ground support can be heavily reduced by employing an inter-satellite link (ISL) communication architecture. Moreover, this concept may provide excellent range rate accuracies in the ISL leveraging on radio link architectures able to suppress the adverse effects of on-board clock instabilities. The constellation entails 5 satellites deployed on three quasi-circular high-altitude polar orbits. The configuration is composed by a main spacecraft in polar orbit and four spacecraft symmetrically located on two inclined orbits. The periodic synchronisation of the constellation clocks with ground is granted by the main spacecraft, the only element of the constellation communicating with Earth. We describe the overall architecture of the constellation and report on the results of our numerical simulations in different operational scenarios. We show that excellent orbital accuracies can be obtained for the constellation using a batch-sequential filter that can be easily implemented on board, thus enabling a high level of navigational autonomy. Furthermore, we analyse the effects of non-gravitational accelerations acting on the satellites and their modelling (based on the SmallSats design being developed in Argotec for Mars/Moon constellations) and assess their effects against the limited computational resources available onboard. The assessment of the achievable positioning accuracy is fundamental to evaluate the feasibility of a future positioning system providing a global coverage of the planet.
Performance analysis of a martian polar navigation system / Molli, S.; Durante, D.; Cascioli, G.; Proietti, S.; Racioppa, P.; Simonetti, S.; Alessi, E. M.; Iess, L.. - B2:(2021), pp. 268-278. (Intervento presentato al convegno IAF Space communications and navigation symposium 2021 at the 72nd International astronautical congress, IAC 2021 tenutosi a Dubai; United Arab Emirates).
Performance analysis of a martian polar navigation system
S. Molli
Primo
;D. Durante;G. Cascioli;S. Proietti;P. Racioppa;L. Iess
2021
Abstract
Deciphering the genesis and evolution of the Martian polar caps can provide critical understanding of Mars’ climate system and allow us to apply the lesson learned on the Earth about planetary climate change on other terrestrial planets. In this work, we present a novel mission concept that can support autonomous navigation of rovers devoted to scientific investigations of these regions. We propose a constellation of 5 small satellites with coverage over Mars polar regions, focusing on the positioning performance that can be obtained. Ground support can be heavily reduced by employing an inter-satellite link (ISL) communication architecture. Moreover, this concept may provide excellent range rate accuracies in the ISL leveraging on radio link architectures able to suppress the adverse effects of on-board clock instabilities. The constellation entails 5 satellites deployed on three quasi-circular high-altitude polar orbits. The configuration is composed by a main spacecraft in polar orbit and four spacecraft symmetrically located on two inclined orbits. The periodic synchronisation of the constellation clocks with ground is granted by the main spacecraft, the only element of the constellation communicating with Earth. We describe the overall architecture of the constellation and report on the results of our numerical simulations in different operational scenarios. We show that excellent orbital accuracies can be obtained for the constellation using a batch-sequential filter that can be easily implemented on board, thus enabling a high level of navigational autonomy. Furthermore, we analyse the effects of non-gravitational accelerations acting on the satellites and their modelling (based on the SmallSats design being developed in Argotec for Mars/Moon constellations) and assess their effects against the limited computational resources available onboard. The assessment of the achievable positioning accuracy is fundamental to evaluate the feasibility of a future positioning system providing a global coverage of the planet.File | Dimensione | Formato | |
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