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  • session 9

    Title

    Modelling and Orbit Determination

    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

    2014-10-01

    Time

    14:45

    Room

    801B

    IPC members
    • Co-Chair: Dr. Heather Cowardin, Jacobs Technology, ESCG, United States;

    • Co-Chair: Mr. Sven Kevin Flegel, European Space Agency (ESA), Germany;

    • Rapporteur: Dr. Hugh G. Lewis, University of Southampton, United Kingdom;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Observation and analysis of the apparent spin period variations of inactive box-wing geosynchronous resident space objects

    18'

    confirmed

    Mr. Michael Earl

    Royal Military College

    Canada

    2

    Results of two year dedicated Molniya-type HEO surveys

    18'

    confirmed

    Dr. Vladimir Agapov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    3

    an orbit determination method of improving parameters by the track direction error based on sparse observation data

    18'

    no-show

    Mr. Dongxu Xing

    BITTT

    China

    4

    Orbit determination of space debris using a bi-static radar configuration with a multiple-beam receiver

    18'

    confirmed

    Mr. Alessandro Morselli

    Politecnico di Milano

    Italy

    5

    Analysis of Assumptions in Debris Environment Evolution Models

    18'

    confirmed

    Dr. David Finkleman

    SkySentry, LLC

    United States

    6

    Disposal strategy for the geosynchronous orbits of the Beidou Navigation Satellite System

    18'

    confirmed

    Dr. Jingshi Tang

    Nanjing University

    China

    7

    Reevaluation of the MASTER-2009 MLI and H-10 Debris Modeling

    18'

    confirmed

    Mr. Sven Kevin Flegel

    Fraunhofer Institute for High Frequency Physics and Radar Techniques (FHR)

    Germany

    8

    A deformation model of flexible, high area-to-mass ratio debris for accurate propagation under perturbations

    18'

    confirmed

    Mr. Sittiporn Channumsin

    School of Engineering, University of Glasgow

    United Kingdom

    9

    Re-entry of spacecraft on highly eccentric orbits - Cluster-II

    18'

    confirmed

    Mr. Ronny Kanzler

    Hypersonic Technology Göttingen

    Germany

    10

    Orbital debris atmospheric re-entry prediction

    18'

    confirmed

    Dr. Jean-Luc VERANT

    Office National d’Etudes et de Recherches Aérospatiales (ONERA)

    France

    Contribution of Ariane H-10 fragmentations to the GTO debris environment

    Mr. Sven Kevin Flegel

    Fraunhofer Institute for High Frequency Physics and Radar Techniques (FHR)

    Germany