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  • session 6

    Title

    Orbital Dynamics (1)

    Description

    This theme discusses advances in the knowledge of natural motions of objects in orbit around the Earth, planets, minor bodies, Lagrangian points and more generally natural orbital dynamics of spacecraft in the Solar System. It also covers advances in orbit determination.

    IPC members
    • Co-Chair: Al Cangahuala, National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory, United States;

    • Co-Chair: Dr. Antonio Prado, National Institute for Space Research - INPE , Brazil;

    • Rapporteur: Dr. Feng-Tai Hwang, National Space Organization, Taipei;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    2

    Leveraging manifolds of tori associated with quasi-satellite orbits to design low-fuel mars-phobos transfers

    10

    confirmed

    Dr. Richard Epenoy

    Centre National d'Etudes Spatiales (CNES)

    France

    3

    A High-order Target Point Approach to the Stationkeeping of Near Rectilinear Halo Orbits

    10

    confirmed

    Mr. XIAOYU FU

    Surrey Space Centre, University of Surrey

    United Kingdom

    4

    Cislunar Transfer Design Exploiting Periodic and Quasi-Periodic Orbital Structures in the Four-Body Problem

    10

    confirmed

    Mr. Brian McCarthy

    Purdue University

    United States

    5

    Orbital Anomaly Reconstruction Using Deep Symbolic Regression

    10

    confirmed

    Mr. Matteo Manzi

    University of Strathclyde

    United Kingdom

    6

    Minimum Cost Relative Dynamics in Cislunar Environment

    10

    confirmed

    Mr. Andrea Capannolo

    Politecnico di Milano

    Italy

    7

    Surface Trajectories of Particles on the Primary of the Sphere-Restricted Full 2-Body Problem

    10

    confirmed

    Dr. Yu Jiang

    State Key Laboratory of Astronautic Dynamics

    China

    8

    Transfers around Phobos using invariant manifolds of unstable Quasi-Satellite Orbits

    10

    confirmed

    Mr. Nishanth Pushparaj

    The Graduate University for Advanced Studies

    Japan

    9

    Closed-Form Solution of Long-Term Invariant Relative Orbit in the Zonal Gravitational Field

    10

    confirmed

    Mr. Yuechen Ma

    Beihang University

    China

    10

    Modelling the break-up and re-entry propagation of meteorites through a continuum approach

    10

    confirmed

    Mr. Simone Limonta

    Politecnico di Milano

    Italy

    11

    An analytic method of the density evolution of large constellations and collision probability evaluation

    10

    confirmed

    Ms. Yidan Gao

    School of Aerospace Engineering, Beijing Institute of Technology

    China

    12

    Accessible Latitudes for Planetary Entry Probe Missions to Saturn, Uranus or Neptune

    10

    confirmed

    Ms. Alena Probst

    Jet Propulsion Laboratory - California Institute of Technology

    United States

    13

    Orbit Determination using Ground-Based Optical Observations in Launch and Early Operations Phase of EDRS-C

    withdrawn

    Dr. Stefan Hackel

    Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

    Germany

    14

    Atmosphere impact assessment on the trajectory control problem for a descent module returning from the Moon

    10

    confirmed

    Mr. Marat Airapetyan

    Bauman Moscow State Technical University

    Russian Federation

    15

    Complex orbit dynamics of decommissioned geostationary satellites

    10

    confirmed

    Mr. Simone Proietti

    Sapienza University of Rome

    Italy