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20112024
most citedAnalytical framework for space debris collision avoidance maneuver design

49 citations · 340 across the 30 of their papers we have counts for

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Showing 2019Show all

9 papers · 1 filter

cs.NE2019★ 30 cited

Spacecraft design optimisation for demise and survivability

Mirko Trisolini, Hugh G. Lewis, Camilla Colombo

Among the mitigation measures introduced to cope with the space debris issue there is the de-orbiting of decommissioned satellites. Guidelines for re-entering objects call for a gr…

astro-ph.IM2019★ 17 cited

Demisability and survivability sensitivity to design-for-demise techniques

Mirko Trisolini, Hugh G. Lewis, Camilla Colombo

The paper is concerned with examining the effects that design-for-demise solutions can have not only on the demisability of components, but also on their survivability that is thei…

astro-ph.EP2019★ 9 cited

Impact probability computation of Near-Earth Objects using Monte Carlo Line Sampling and Subset Simulation

Matteo Romano, Matteo Losacco, Camilla Colombo +1

This work introduces two Monte Carlo (MC)-based sampling methods, known as line sampling and subset simulation, to improve the performance of standard MC analyses in the context of…

astro-ph.EP2019★ 1 cited

Stable attitude dynamics of planar helio-stable and drag-stable sails

Narcís Miguel, Camilla Colombo

In this paper the planar orbit and attitude dynamics of an uncontrolled spacecraft is studied, taking on-board a deorbiting device. Solar and drag sails with the same shape are con…

physics.space-ph2019★ 12 cited

Coverage Area Determination for Conical Fields of View Considering an Oblate Earth

Marco Nugnes, Camilla Colombo, Massimo Tipaldi

This paper introduces a new analytical method for the determination of the coverage area modeling the Earth as an oblate ellipsoid of rotation. Starting from the knowledge of the s…

astro-ph.EP2019★ 12 cited

Extension of the King-Hele orbit contraction method for accurate, semi-analytical propagation of non-circular orbits

Stefan Frey, Camilla Colombo, Stijn Lemmens

Numerical integration of orbit trajectories for a large number of initial conditions and for long time spans is computationally expensive. Semi-analytical methods were developed to…