International audienceThis paper aims at investigating the stability over 150 years of a very large number of trajectories in the Medium Earth Orbit (MEO) region, near the orbits devoted to radionavigation such as the Global Navigation Satellite Systems (GNSS like GPS, Glonass, Galileo, COMPASS). The stability is characterized by the long term evolution of the eccentricity, and a stable orbit will be defined by initial conditions not inducing through gravitational perturbations a high difference between the perigee and apogee altitudes over a 150 years (for keeping as low as possible the collision risk with operational orbits). The initial conditions of motion used for our tests cover a wide range of semi-major axes and inclinations, regula...
This paper investigates the long-term evolution of spacecraft in Highly Elliptical Orbits (HEOs). Th...
The growth of the population of space debris in the geostationary ring and the resulting threat to a...
The dynamical evolution of objects released in geostationary orbit with area-to-mass ratios (A/M) be...
International audienceThis paper aims at investigating the stability over 150 years of a very large ...
International audienceThis paper aims at investigating the stability over 200 years of a very large ...
We present the results of an extensive numerical exploration performed on the eccentricity growth in...
This paper investigates the long-term evolution of spacecraft in Highly Elliptical Orbits (HEOs). Th...
Through the averaged equations we revisit theoretical and numerical aspects of the strong resonance ...
International audienceIn the last decades the important increase of the number of positioning satell...
Through the averaged equations we revisit theoretical and numerical aspects of the strong resonance ...
Recent studies have shown that the medium-Earth orbit (MEO) region of the global navigation satellit...
The aim of this work is to investigate the main dominant terms of lunisolar perturbations that affec...
With currently two constellations being in or close to the build-up phase, in a few years the Medium...
The long-term dynamics of the geostationary Earth orbits (GEO) is revisited through the application ...
We have carried out a numerical investigation of the coupled gravitational and non-gravitational per...
This paper investigates the long-term evolution of spacecraft in Highly Elliptical Orbits (HEOs). Th...
The growth of the population of space debris in the geostationary ring and the resulting threat to a...
The dynamical evolution of objects released in geostationary orbit with area-to-mass ratios (A/M) be...
International audienceThis paper aims at investigating the stability over 150 years of a very large ...
International audienceThis paper aims at investigating the stability over 200 years of a very large ...
We present the results of an extensive numerical exploration performed on the eccentricity growth in...
This paper investigates the long-term evolution of spacecraft in Highly Elliptical Orbits (HEOs). Th...
Through the averaged equations we revisit theoretical and numerical aspects of the strong resonance ...
International audienceIn the last decades the important increase of the number of positioning satell...
Through the averaged equations we revisit theoretical and numerical aspects of the strong resonance ...
Recent studies have shown that the medium-Earth orbit (MEO) region of the global navigation satellit...
The aim of this work is to investigate the main dominant terms of lunisolar perturbations that affec...
With currently two constellations being in or close to the build-up phase, in a few years the Medium...
The long-term dynamics of the geostationary Earth orbits (GEO) is revisited through the application ...
We have carried out a numerical investigation of the coupled gravitational and non-gravitational per...
This paper investigates the long-term evolution of spacecraft in Highly Elliptical Orbits (HEOs). Th...
The growth of the population of space debris in the geostationary ring and the resulting threat to a...
The dynamical evolution of objects released in geostationary orbit with area-to-mass ratios (A/M) be...