Publicaciones en colaboración con investigadores/as de University of Southampton (19)

2016

  1. Re-entry prediction of spent rocket bodies in gto

    Spaceflight mechanics 2016, pts i-iv

2015

  1. A high order method for orbital conjunctions analysis: Monte Carlo collision probability computation

    Advances in Space Research, Vol. 55, Núm. 1, pp. 311-333

  2. A new high sensitivity radar sensor for space debris detection and accurate orbit determination

    2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings, pp. 562-567

  3. A semi-analytical guidance algorithm for autonomous landing

    Advances in Space Research, Vol. 152, Núm. 11, pp. 731-746

  4. Density of debris fragments through differential algebra and averaged dynamics

    Spaceflight mechanics 2015, pts i-iii

  5. Efficient evaluation of vapour-liquid equilibria from multi-parameter thermodynamic models using differential algebra

    Journal of Computational and Applied Mathematics, Vol. 273, pp. 404-413

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

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

  7. End-of-life disposal of libration point orbit missions: The case of Gaia

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

  8. High order transfer maps for perturbed Keplerian motion

    Celestial mechanics and dynamical astronomy, Vol. 122, Núm. 4, pp. 333-358

  9. IAC-15-A6.4.8 The design and optimisation of end-of-life disposal manoeuvres for gnss spacecraft: The case of galileo

    Proceedings of the International Astronautical Congress, IAC, pp. 2187-2199

  10. Impact of high-risk conjunctions on Active Debris Removal target selection

    Advances in Space Research, Vol. 56, Núm. 8, pp. 1752-1764

  11. Long term nonlinear propagation of uncertainties in perturbed geocentric dynamics using automatic domain splitting

    Advances in the Astronautical Sciences, Vol. 153, pp. 473-492

  12. Multi-step optimization strategy for fuel-optimal orbital transfer of low-thrust spacecraft

    Engineering Optimization

  13. Propagation of large uncertainty sets in orbital dynamics by automatic domain splitting

    Celestial mechanics and dynamical astronomy, Vol. 122, Núm. 3, pp. 239-261