A scalable second-order analytical orbit propagator programme based on modern and classical perturbation methods is being developed. As a first step in the validation and verification of part of our orbit propagator programme, we only consider the perturbation produced by zonal harmonic coefficients in the Earth's gravity potential, so that it is possible to analyze the behaviour of the mathematical expressions involved in Delaunay normalization and the Krylov-Bogoliubov-Mitropolsky method in depth and determine their limits. © 2014 David Ortigosa et al
Analytical integration in Artificial Satellite Theory may benefit from different canonical simplific...
A geostationary transfer orbit (GTO) is typically used to inject spacecraft into the geosta- tionary...
Two new intermediary orbits of the artificial satellite problem are proposed. The analytical solutio...
A scalable second-order analytical orbit propagator programme based on modern and classical perturba...
When the elimination of the parallax and the elimination of the perigee is applied to the zonal prob...
Abstract. Using the elimination of the parallax followed by the Delaunay normalization, we present a...
In year 2000 a house-made orbital propagator was developed by the SDG-UPM (former Grupo de Dinámica ...
This article provides a method for finding initial conditions for perturbed frozen orbits around inh...
Abstract. Using the elimination of the parallax followed by the Delaunay normalization, we present a...
Classical procedures for designing Earth's mapping missions rely on a preliminary frozen-eccentricit...
This article provides a method for finding initial conditions for perturbed frozen orbits around inh...
Four widely used algorithms for the computation of the Earth's gravitational potential and its first...
Determining higher order perturbations for lunar orbiter by Krylov-Bololiubov and Poincare method
In year 2000 a house-made orbital propagator was developed by the SDG-UPM (former Grupo de Dinámica ...
The selection of orbit propagation models strongly affects various space situational awareness appli...
Analytical integration in Artificial Satellite Theory may benefit from different canonical simplific...
A geostationary transfer orbit (GTO) is typically used to inject spacecraft into the geosta- tionary...
Two new intermediary orbits of the artificial satellite problem are proposed. The analytical solutio...
A scalable second-order analytical orbit propagator programme based on modern and classical perturba...
When the elimination of the parallax and the elimination of the perigee is applied to the zonal prob...
Abstract. Using the elimination of the parallax followed by the Delaunay normalization, we present a...
In year 2000 a house-made orbital propagator was developed by the SDG-UPM (former Grupo de Dinámica ...
This article provides a method for finding initial conditions for perturbed frozen orbits around inh...
Abstract. Using the elimination of the parallax followed by the Delaunay normalization, we present a...
Classical procedures for designing Earth's mapping missions rely on a preliminary frozen-eccentricit...
This article provides a method for finding initial conditions for perturbed frozen orbits around inh...
Four widely used algorithms for the computation of the Earth's gravitational potential and its first...
Determining higher order perturbations for lunar orbiter by Krylov-Bololiubov and Poincare method
In year 2000 a house-made orbital propagator was developed by the SDG-UPM (former Grupo de Dinámica ...
The selection of orbit propagation models strongly affects various space situational awareness appli...
Analytical integration in Artificial Satellite Theory may benefit from different canonical simplific...
A geostationary transfer orbit (GTO) is typically used to inject spacecraft into the geosta- tionary...
Two new intermediary orbits of the artificial satellite problem are proposed. The analytical solutio...