Juan Félix San Juan Díaz-rekin lankidetzan egindako argitalpenak (34)

2024

  1. Vectorial formulation for the propagation of average dynamics under gravitational effects

    Acta Astronautica, Vol. 217, pp. 181-187

2023

  1. Vectorial formulation for the propagation of average dynamics under gravitational effects

    Proceedings of the International Astronautical Congress, IAC

2022

  1. KePASSA-22. 5th International Workshop on Key Topics in Orbit Propagation applied to Space Situational Awareness: Program & Abstract Book

    Universidad de La Rioja

2020

  1. Exploring the long-term dynamics of perturbed Keplerian motion in high degree potential fields

    Communications in Nonlinear Science and Numerical Simulation, Vol. 82

2018

  1. A parametric study of the orbital lifetime of super GTO and SSTO orbits based on semi-analytical integration

    Astrophysics and Space Science Proceedings. Stardust Final Conference (Springer), pp. 85-98

  2. HEOSAT: a mean elements orbit propagator program for highly elliptical orbits

    CEAS Space Journal, Vol. 10, Núm. 1, pp. 3-23

2015

  1. End-of-life disposal of high elliptical orbit missions: The case of INTEGRAL

    Advances in Space Research, Vol. 56, Núm. 3, pp. 479-493

2014

  1. Delaunay variables approach to the elimination of the perigee in Artificial Satellite Theory

    Celestial mechanics and dynamical astronomy, Vol. 120, Núm. 1, pp. 39-56

  2. Efficient semi-analytic integration of GNSS orbits under tesseral effects

    Acta Astronautica, Vol. 102, pp. 355-366

  3. Long-term evolution of Galileo operational orbits by canonical perturbation theory

    Acta Astronautica, Vol. 94, Núm. 2, pp. 646-655

  4. Proper averaging via parallax elimination

    Advances in the Astronautical Sciences, Vol. 150, pp. 315-331

2013

  1. Averaging tesseral effects: Closed form relegation versus expansions of elliptic motion

    Mathematical Problems in Engineering, Vol. 2013, pp. 1-11

  2. Precise analytical computation of frozen-eccentricity, low earth orbits in a tesseral potential

    Mathematical Problems in Engineering, Vol. 2013, pp. 1-13

2012

  1. COMPARISON OF DELAUNAY NORMALIZATION AND THE KRYLOV-BOGOLIUBOV-MITROPOLSKY METHOD

    SPACEFLIGHT MECHANICS 2012

  2. On bounded satellite motion under constant radial propulsive acceleration

    Mathematical Problems in Engineering, Vol. 2012, pp. 1-13

  3. On the third-body perturbations of high-altitude orbits

    Celestial mechanics & dynamical astronomy, Vol. 113, Núm. 4, pp. 435-452

  4. Semianalytic integration of high-altitude orbits under lunisolar effects

    Mathematical Problems in Engineering, Vol. 2012, pp. 1-18

2011

  1. Deep resonant GPS-Dynamics due to the geopotential

    Journal of the Astronautical Sciences, Vol. 58, Núm. 4, pp. 661-676

  2. Long-term evolution of Galileo operational orbits by canonical perturbation theory

    62nd International Astronautical Congress 2011, IAC 2011, pp. 4815-4825

  3. Using the DSST semi-analytical orbit propagator package via the nondywebtools/astrodywebtools open science environment

    62nd International Astronautical Congress 2011, IAC 2011, pp. 4337-4344