The growth of the population of space debris in the geostationary ring and the resulting threat to active satellites require insight into the dynamics of uncontrolled objects in the region. A Monte Carlo simulation analyzed the sensitivity to initial conditions of the long-term evolution of geostationary spacecraft near an unstable point of the geopotential, where irregular behavior (e.g., transitions between long libration and continuous circulation) occurs. A statistical analysis unveiled sudden transitions from order to disorder, interspersed with intervals of smooth evolution. There is a periodicity of approximately half a century in the episodes of disorder, suggesting a connection with the precession of the orbital plane, due to Earth...
The long-term evolution, over 54 years, of a sample of objects released in geostationary orbit with ...
This thesis explores the dynamical evolution of celestial bodies, both natural and artificial, which...
In this work, we exploit the luni-solar perturbations for the post-mission disposal of satellites in...
The growth of the population of space debris in the geostationary ring and the resulting threat to a...
The long-term dynamics of the geostationary Earth orbits (GEO) is revisited through the application ...
International audienceThis paper aims at investigating the stability over 200 years of a very large ...
The dynamical evolution of objects released in geostationary orbit with area-to-mass ratios (A/M) be...
In nominal mission scenarios, geostationary satellites perform end-of-life orbit maneuvers to reach ...
We have carried out a numerical investigation of the coupled gravitational and non-gravitational per...
We consider Earth satellite orbits in the range of semimajor axes where the perturbing effects of Ea...
This paper investigates the long-term evolution of spacecraft in Highly Elliptical Orbits (HEOs). Th...
International audienceThis paper aims at investigating the stability over 150 years of a very large ...
Context. Close satellite orbits around small and elongated celestial bodies can experience massive a...
Faculty Advisor: Dr. Richard LinaresThis research was supported by the Undergraduate Research Opport...
The aim of this work is to investigate the main dominant terms of lunisolar perturbations that affec...
The long-term evolution, over 54 years, of a sample of objects released in geostationary orbit with ...
This thesis explores the dynamical evolution of celestial bodies, both natural and artificial, which...
In this work, we exploit the luni-solar perturbations for the post-mission disposal of satellites in...
The growth of the population of space debris in the geostationary ring and the resulting threat to a...
The long-term dynamics of the geostationary Earth orbits (GEO) is revisited through the application ...
International audienceThis paper aims at investigating the stability over 200 years of a very large ...
The dynamical evolution of objects released in geostationary orbit with area-to-mass ratios (A/M) be...
In nominal mission scenarios, geostationary satellites perform end-of-life orbit maneuvers to reach ...
We have carried out a numerical investigation of the coupled gravitational and non-gravitational per...
We consider Earth satellite orbits in the range of semimajor axes where the perturbing effects of Ea...
This paper investigates the long-term evolution of spacecraft in Highly Elliptical Orbits (HEOs). Th...
International audienceThis paper aims at investigating the stability over 150 years of a very large ...
Context. Close satellite orbits around small and elongated celestial bodies can experience massive a...
Faculty Advisor: Dr. Richard LinaresThis research was supported by the Undergraduate Research Opport...
The aim of this work is to investigate the main dominant terms of lunisolar perturbations that affec...
The long-term evolution, over 54 years, of a sample of objects released in geostationary orbit with ...
This thesis explores the dynamical evolution of celestial bodies, both natural and artificial, which...
In this work, we exploit the luni-solar perturbations for the post-mission disposal of satellites in...