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  • session 6

    Title

    Guidance, Navigation and Control (2)

    Description

    The emphasis of this theme is on the studies and application related to the guidance, navigation and control of Earth-orbiting and interplanetary spacecraft and rockets, including formation flying, rendezvous and docking.

    Date

    2014-10-02

    Time

    09:45

    Room

    801A

    IPC members
    • Co-Chair: Dr. Bernard Lübke-Ossenbeck, OHB System AG-Bremen, Germany;

    • Co-Chair: Mrs Benedicte Escudier, Institut Supérieur de l'Aéronautique et de l'Espace (ISAE), France;

    • Rapporteur: Prof. Fuyuto Terui, Kanagawa Institute of Technology, Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    characteristic model based golden section phase plane adaptive control method and its application in rendezvous and docking

    15'

    confirmed

    Prof. YongChun Xie

    Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)

    China

    2

    PRISMA IRIDES: Close Range Optical Inspection of the non-cooperative Satellite Picard

    15'

    withdrawn

    Mr. Thomas Karlsson

    OHB Sweden

    Sweden

    3

    adaptive finite time control of relative translation in proximity of a freely tumbling spacecraft

    15'

    confirmed

    Dr. Shunan Wu

    Dalian University of Technology (DUT)

    China

    4

    Development of an Integrated Spacecraft Guidance, Navigation, & Control Subsystem for Automated Proximity Operations

    15'

    confirmed

    Mr. Peter Schulte

    School of Aerospace Engineering, Georgia Institute of Technology

    United States

    5

    A testbed for visual based navigation and control during space rendezvous operations

    15'

    confirmed

    Dr. Marco Sabatini

    Sapienza University of Rome

    Italy

    6

    Low-Earth Orbit Spacecraft Relative orbit and attitude decentralized estimation.

    15'

    withdrawn

    Mr. Adolfo Chaves Jimenez

    Delft University of Technology (TU Delft)

    The Netherlands

    7

    Relative Navigation State Estimation Performance for Orbit Debris Removal and Deep-Space Rendezvous

    15'

    confirmed

    Dr. Jean-Francois Hamel

    NGC Aerospace Ltd.

    Canada

    8

    Robust Tether Deployment Control for Electrodynamic Tether Deorbit System

    15'

    no-show

    Dr. Feng Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    9

    Towing tethers to control debris removal dynamics

    15'

    confirmed

    Mr. Riccardo Benvenuto

    Politecnico di Milano

    Italy

    10

    Controllability of a Square Solar Sail with Movable Membrane Tips

    15'

    confirmed

    Mr. Bo Fu

    United States

    11

    analytical three-phase transfer to a solar polar orbit using solar sail propulsion

    15'

    confirmed

    Ms. Ciara McGrath

    University of Strathclyde/Advanced Space Concepts Laboratory

    United Kingdom

    12

    optimal spin rate control of a spinning solar sail for orbital inclination change

    15'

    confirmed

    Mr. Go Ono

    University of Tokyo

    Japan

    13

    A feasibility study of solar radiation pressure feedback control strategy for unstable periodic orbits in the restricted three-body problem

    15'

    confirmed

    Ms. Stefania Soldini

    University of Southampton

    United Kingdom