Analysis of the orbital evolution of space debris using a solar sail and natural forces
Jean Paulo dos S. Carvalho, Rodolpho Vilhena de Moraes, Antonio, Fernando Bertachini de A. Prado

TL;DR
This paper models the orbital evolution of GEO space debris considering natural forces and introduces a novel SRP model accounting for the Sun's elliptical orbit, demonstrating the potential of solar sails for space debris mitigation.
Contribution
Develops a new SRP model considering the Sun's elliptical orbit and identifies initial conditions that amplify eccentricity growth, aiding space debris removal strategies.
Findings
First-order SRP term dominates over second-order.
Certain initial conditions significantly increase eccentricity.
Solar sails can effectively assist in space debris cleanup.
Abstract
In this work, the orbital evolution of these objects that are located in the geostationary orbit (GEO) is analyzed. Knowing this, the possibility of using a solar sail is considered to help to clean the space environment. The main natural environmental perturbations that act in the orbit of the debris are considered in the dynamics. Such forces acting in the solar sail can force the growth of the eccentricity of these objects in the GEO orbit. Several authors have presented models of the solar radiation pressure considering the single-averaged model. But, doing a literature research, we found that the authors consider the Earth around the Sun in a circular and inclined orbit. Our contribution to the SRP model is in developing a different approach from other authors, where we consider the Sun in an elliptical and inclined orbit, which is valid for other bodies in the solar system when…
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Taxonomy
TopicsSpace Satellite Systems and Control · Astro and Planetary Science · Spacecraft Dynamics and Control
