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20112023
most citedAssessing and Minimizing Collisions in Satellite Mega-Constellations

50 citations · 121 across the 9 of their papers we have counts for

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6 papers · 1 filter

astro-ph.EP2022

Near-Linear Orbit Uncertainty Propagation in the Perturbed Two-Body Problem

Javier Hernando-Ayuso, Claudio Bombardelli, Giulio Baù +1

The paper addresses the problem of minimizing the impact of non-linearities when dealing with uncertainty propagation in the perturbed two-body problem. The recently introduced gen…

astro-ph.EP2021★ 1 cited

A generalization of the equinoctial orbital elements

Giulio Baù, Javier Hernando-Ayuso, Claudio Bombardelli

We introduce six quantities that generalize the equinoctial orbital elements when some or all the perturbing forces that act on the propagated body are derived from a disturbing po…

astro-ph.EP2020

Space Occupancy in Low-Earth Orbit

Claudio Bombardelli, Gabriele Falco, Davide Amato +1

With the upcoming launch of large constellations of satellites in the low-Earth orbit (LEO) region it will become important to organize the physical space occupied by the different…

astro-ph.EP2020★ 50 cited

Assessing and Minimizing Collisions in Satellite Mega-Constellations

Nathan Reiland, Aaron J. Rosengren, Renu Malhotra +1

We aim to provide satellite operators and researchers with an efficient means for evaluating and mitigating collision risk during the design process of mega-constellations. We firs…

astro-ph.EP2019★ 9 cited

Multiple Scales Asymptotic Solution For The Constant Radial Thrust Problem

Juan Luis Gonzalo, Claudio Bombardelli

An approximate analytical solution for the two body problem perturbed by a radial, low acceleration is obtained, using a regularized formulation of the orbital motion and the metho…

astro-ph.EP2018★ 26 cited

Non-averaged regularized formulations as an alternative to semi-analytical orbit propagation methods

Davide Amato, Claudio Bombardelli, Giulio Baù +2

This paper is concerned with the comparison of semi-analytical and non-averaged propagation methods for Earth satellite orbits. We analyse the total integration error for semi-anal…