activity
20112023
most citedAssessing and Minimizing Collisions in Satellite Mega-Constellations

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

collaborators

10 papers

math.OC2023

Convex Optimization-Based Model Predictive Control for the Guidance of Active Debris Removal Transfers

Minduli Wijayatunga, Roberto Armellin, Harry Holt +2

Active debris removal (ADR) missions have garnered significant interest as means of mitigating collision risks in space. This work proposes a convex optimization-based model predic…

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…