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  • 7-A6.10
  • session 7-A6.10

    Title

    Orbital Safety and Optimal Operations in an Increasingly Congested Environment (Joint Astrodynamics/Space Debris Session)

    Description

    This joint session will concern itself with the technical challenges driven by salient problems in space debris and space traffic that can be well informed by contributions from the field of astrodynamics (the science that studies the motion of objects in space). Specific issues regarding long-term population assessments and predictions, safely operating NextGen (large) Constellations, determining the data and modeling requirements to uniquely identify and predict the motion of objects in space (e.g. class specific), discovering and developing improved methods of debris mitigation and remediation founded upon forces and torques, development of semi-analytical theories relevant to specific classes and types of orbital debris, etc. are of relevance to this joint session.

    Date

    2018-10-04

    Time

    14:45

    Room

    CCB Borgward

    IPC members
    • Co-Chair: Dr. Yukihito Kitazawa, JAXA, Japan;

    • Co-Chair: Dr. A. K. Anil Kumar, Indian Space Research Organization (ISRO), India;

    • Rapporteur: Prof. Moriba Jah, Privateer Space, Inc., United States;

    • Rapporteur: Prof. Daniel Scheeres, Colorado Center for Astrodynamics Research, University of Colorado, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    GOES 8 Tumbling Spin State Evolution and the Implications for GEO Debris Mitigation

    15

    confirmed

    Mr. Conor Benson

    Colorado Center for Astrodynamics Research, University of Colorado

    United States

    2

    Uncertainty and Data Observability Analysis for RSO Mass/Albedo-Area Estimation

    15

    confirmed

    Mr. Vishnuu Mallik

    The University of Texas at Austin

    United States

    3

    Long-term dynamical evolution analysis and luni-solar resonances for inclined geostationary transfer orbits

    15

    confirmed

    Prof. Haichao Gui

    Beihang University

    China

    4

    Automated near real-time validation and exploitation of optical sensor data for improved orbital safety

    15

    confirmed

    Dr. Thomas Kelecy

    Applied Defense Solutions, Inc.

    United States

    5

    Using Reachability to Compute Unsafe Regions in State Space through Sampling Methods

    15

    confirmed

    Mr. Julian Brew

    Georgia Institute of Technology

    United States

    6

    Rapid Modeling of Electrostatic Forces and Torques Considering Dielectrics

    15

    confirmed

    Mr. Joseph Hughes

    University of Colorado Boulder

    United States

    7

    Debris Collision Avoidance by means of Attitude Control - in flight demonstration with TET-1

    15

    confirmed

    Ms. Maren Huelsmann

    DLR (German Aerospace Center)

    Germany

    8

    Evolution of Fragmentation Cloud in Highly Eccentric Earth Orbits through Continuum Modelling

    15

    confirmed

    Mr. Stefan Frey

    Politecnico di Milano

    Italy

    9

    LEDSAT: a LED-based LEO demonstrator for space debris orbit and attitude determination

    15

    confirmed

    Mr. Paolo Marzioli

    Sapienza University of Rome

    Italy

    10

    The concept of the functioning of a space vehicle - a space debris collector with a view to removing objects of space debris into orbit of a burial

    15

    confirmed

    Dr. Vsevolod Koryanov

    Bauman Moscow State Technical University

    Russian Federation

    11

    Dynamical system description of the solar radiation pressure and J2 phase space for end-of-life design and frozen orbit design

    15

    confirmed

    Dr. Elisa Maria Alessi

    IFAC-CNR

    Italy

    12

    Low Thrust Manoeuvre Detection for Low Earth Orbit Space Objects

    15

    confirmed

    Dr. Steve Gehly

    University of New South Wales

    Australia