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  • session 9

    Title

    Orbit Determination and Propagation

    Description

    This session will address aspects of space debris orbit determination related to assessment of raw and derived data accuracy, optical measurements processing and modelling and risk analysis of space debris.

    Date

    2018-10-03

    Time

    14:45

    Room

    ZARM 1

    IPC members
    • Co-Chair: Dr. Seishiro Kibe, Japan Aerospace Exploration Agency (JAXA), Japan;

    • Co-Chair: Dr. Annamaria Nassisi, Thales Alenia Space Italia, Italy;

    • Rapporteur: Prof.Dr. Heiner Klinkrad, European Space Agency (ESA), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    General Perturbations Methods for Orbit Propagation with Particular Application to Space Debris Mitigation Compliance

    18

    confirmed

    Ms. Emma Kerr

    Space Environment Research Centre Ltd. (SERC); School of Science, RMIT University

    Australia

    2

    Impact of variations in thermospheric mass density on the orbit propagation of low Earth orbit satellites

    18

    confirmed

    Mr. Changyong HE

    RMIT University (Royal Melbourne Institute of Technology)

    Australia

    3

    Towards the maintenance of Gaussianity on state vector uncertainty propagation

    18

    confirmed

    Mr. Juan Carlos Dolado Perez

    Centre National d'Etudes Spatiales (CNES)

    France

    4

    Filtering under ambiguity for the debris-tracking problem

    18

    confirmed

    Mr. Shambo Bhattacharjee

    University of Leeds

    United Kingdom

    5

    Validation of a novel coupled orbit-attitude propagator by comparison to SLR data and light curves

    18

    confirmed

    Mr. Luc Sagnieres

    McGill University

    Canada

    6

    Reconstruction of Non-Cooperative Spacecraft Maneuvers During Observation Gaps From Angles-Only Measurements Using Machine Learning

    18

    confirmed

    Mr. Jason Reiter

    Pennsylvania State University

    United States

    7

    Using Conjunction Analysis Methods for Manoeuvre Detection - Application to Optical Observations

    18

    confirmed

    Dr. Johannes Herzog

    Deutsches Zentrum fuer Luft- und Raumfahrt (DLR)

    Germany

    8

    Improving accuracy of LEO objects Two-Line Elements through optical measurements

    18

    confirmed

    Mr. Marco Acernese

    Sapienza University of Rome

    Italy

    9

    Object Detection Methods for Radar Survey Measurements

    18

    confirmed

    Mr. Alejandro Pastor-Rodríguez

    GMV Aerospace & Defence SAU

    Spain

    10

    Comparison of New Methods for the Correlation of Short Radar Tracklets

    18

    confirmed

    Mr. Benedikt Reihs

    Astronomical Institute University of Bern (AIUB)

    Switzerland