Publicaciones en colaboración con investigadores/as de Real Instituto y Observatorio de la Armada (54)

2012

  1. Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects

    Journal of Aerospace Engineering, Sciences and Applications

  2. J2-perturbation solution to the relative motion problem

    Advances in the Astronautical Sciences

  3. Modifying the atlas of low lunar orbits using inert tethers

    Acta Astronautica

  4. On roto-translatory motion: Reductions and radial intermediaries

    Journal of the Astronautical Sciences

  5. Periodic orbits of a Hill-tether problem originated from collinear points

    Journal of Guidance, Control, and Dynamics, Vol. 35, Núm. 1, pp. 222-233

2011

  1. Ceres' rotation solution under the gravitational torque of the Sun

    Monthly Notices of the Royal Astronomical Society, Vol. 415, Núm. 1, pp. 461-469

  2. Design of long-lifetime lunar orbits: A hybrid approach

    Acta Astronautica, Vol. 69, Núm. 3-4, pp. 186-199

  3. Planetary dynamics in binary systems: A qualitative analysis of the S-type case

    AIP Conference Proceedings

2010

  1. Analytical theory for spacecraft motion about Mercury

    Acta Astronautica, Vol. 66, Núm. 7-8, pp. 1022-1038

  2. Fast computation of low lunar frozen orbits in a high degree Selenopotential

    Advances in the Astronautical Sciences

  3. First-order rotation solution of an oblate rigid body under the torque of a perturber in circular orbit

    Astronomy and Astrophysics, Vol. 519

  4. Integration of the rotation of an earth-like body as a perturbed spherical rotor

    Astronomical Journal, Vol. 139, Núm. 5, pp. 1899-1908

  5. New elements for the efficient propagation of attitude dynamics

    61st International Astronautical Congress 2010, IAC 2010

2009

  1. Hill problem analytical theory to the order four: Application to the computation of frozen orbits around planetary satellites

    Mathematical Problems in Engineering, Vol. 2009

  2. Lunar analytical theory for polar orbits in a 50-degree zonal model plus third-body effect

    Journal of the Astronautical Sciences

  3. On the design of an Enceladus science orbit

    Acta Astronautica, Vol. 65, Núm. 1-2, pp. 27-39

2008

  1. Analytical theory for spacecraft motion about Mercury

    International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008

  2. Computing long-lifetime Science orbits around natural satellites

    Discrete and Continuous Dynamical Systems - Series S, Vol. 1, Núm. 2, pp. 293-302

  3. Fast design of repeat ground track orbits in high-fidelity geopotentials

    Journal of the Astronautical Sciences, Vol. 56, Núm. 3, pp. 311-324

  4. Io exploration with electrodynamic tethers

    AIAA/AAS Astrodynamics Specialist Conference and Exhibit