Add to ORKGIn the present work it is presented a semi-analytical and a numerical study of the perturbation caused in a spacecraft by a third body using a double averaged analytical model with the disturbing function expanded in Legendre polynomials up to the second-order. The important reason for this procedure is to eliminate the terms due to the short time periodic motion of the spacecraft and to show smooth curves for the evolution of the mean orbital elements for a long time period. The aim of this study is to calculate the effect of lunar perturbations on the orbits of spacecrafts that are traveling around the Earth. It is presented an analysis of the stability of a near-circular orbit and a study to know under which conditions this orbit remains...
In this work we study the dynamics of fictitious satellites of the Earth. In the first part we do no...
An analytical method is investigated to evaluate the low-thrust orbit dynamics of a spacecraft under...
This paper intends to highlight the effect of the third-body in an inclined orbit on a spacecraft or...
This work presents a semi-analytical and numerical study of the perturbation caused in a spacecraft ...
The equations for the variations of the Keplerian elements of the orbit of a spacecraft perturbed by...
In the present work, we expanded the study done by Solorzanol(1) including the eccentricity of the p...
In this paper we present an analytical theory with numerical simulations to study the orbital motion...
This paper develops a semi-analytical study of the perturbation caused to a spacecraft by a third bo...
We present here the first numerical results of our analytical theory of an artificial satellite of t...
The effects of a third-body travelling in a circular orbit around a main body on a massless satellit...
The Lagrange’s planetary equations written in terms of the classical orbital elements have the disad...
ArXiv e-prints. may 1 2016. vol. 1605.When dealing with satellites orbiting a central body on a high...
The determination of analytical expressions which, including the main perturbative effects, allow th...
Some orbital characteristics of lunar artificial satellites is presented taking into account the per...
The long-term effects of a distant third-body on a massless satellite that is orbiting an oblate bod...
In this work we study the dynamics of fictitious satellites of the Earth. In the first part we do no...
An analytical method is investigated to evaluate the low-thrust orbit dynamics of a spacecraft under...
This paper intends to highlight the effect of the third-body in an inclined orbit on a spacecraft or...
This work presents a semi-analytical and numerical study of the perturbation caused in a spacecraft ...
The equations for the variations of the Keplerian elements of the orbit of a spacecraft perturbed by...
In the present work, we expanded the study done by Solorzanol(1) including the eccentricity of the p...
In this paper we present an analytical theory with numerical simulations to study the orbital motion...
This paper develops a semi-analytical study of the perturbation caused to a spacecraft by a third bo...
We present here the first numerical results of our analytical theory of an artificial satellite of t...
The effects of a third-body travelling in a circular orbit around a main body on a massless satellit...
The Lagrange’s planetary equations written in terms of the classical orbital elements have the disad...
ArXiv e-prints. may 1 2016. vol. 1605.When dealing with satellites orbiting a central body on a high...
The determination of analytical expressions which, including the main perturbative effects, allow th...
Some orbital characteristics of lunar artificial satellites is presented taking into account the per...
The long-term effects of a distant third-body on a massless satellite that is orbiting an oblate bod...
In this work we study the dynamics of fictitious satellites of the Earth. In the first part we do no...
An analytical method is investigated to evaluate the low-thrust orbit dynamics of a spacecraft under...
This paper intends to highlight the effect of the third-body in an inclined orbit on a spacecraft or...