All Stories

  1. Orbital Element Reachable Set After Gravity Assists of Planets in Elliptical Orbits

    Article • Journal of Guidance Control and Dynamics, May 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Changxuan Wen

  2. Reachable domain for satellite relative motion along elliptic orbit with uncertainty and process noise

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, January 2020, SAGE Publications

    Dr Changxuan Wen

  3. Reachable Domain of Spacecraft After a Gravity-Assist Flyby

    Article • Journal of Guidance Control and Dynamics, April 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Changxuan Wen

  4. Reachable domain for spacecraft with ellipsoidal Delta-V distribution

    Article • Astrodynamics, June 2018, Tsinghua University Press

    Dr Changxuan Wen

  5. Three-dimensional relative reachable domain with initial state uncertainty in Gaussian distribution

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, February 2018, SAGE Publications

    Dr Changxuan Wen

  6. Guidance, navigation and control for autonomous R-bar proximity operations for geostationary satellites

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, March 2017, SAGE Publications

    Dr Changxuan Wen

  7. Modeling Early Medium-Term Evolution of Debris Clouds Using the Reachable Domain Method

    Article • Journal of Guidance Control and Dynamics, December 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Changxuan Wen, Pini Gurfil

  8. Relative Reachable Domain for Spacecraft with Initial State Uncertainties

    Article • Journal of Guidance Control and Dynamics, March 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Changxuan Wen, Pini Gurfil

  9. Assessing Nanosatellite Cluster Launch Scenarios

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Changxuan Wen

  10. Precise Determination of Reachable Domain for Spacecraft with Single Impulse

    Article • Journal of Guidance Control and Dynamics, November 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Changxuan Wen

  11. Orbital Accessibility Problem for Spacecraft with a Single Impulse

    Article • Journal of Guidance Control and Dynamics, July 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Hao Zhang, Dr Changxuan Wen

  12. Derivative Analysis and Algorithm Modification of Transverse-Eccentricity-Based Lambert Problem

    Article • Journal of Guidance Control and Dynamics, July 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Changxuan Wen

  13. Solving the relative Lambert's problem and accounting for its singularities

    Article • Acta Astronautica, April 2014, Elsevier

    Dr Changxuan Wen