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  • session 2

    Title

    Guidance, Navigation & 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

    2016-09-27

    Time

    09:45

    Room

    Salon Jalisco E6

    IPC members
    • Co-Chair: Dr. Shoji Yoshikawa, Mitsubishi Electric Corporation, Japan;

    • Co-Chair: Prof. Moriba Jah, The University of Texas at Austin, United States;

    • Rapporteur: Dr. Stephan Theil, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Mapping asteroid surfaces with rover swarms

    15'

    confirmed

    Mr. William Crowe

    UNSW Australia

    Australia

    2

    HIL testing of a vision-based autonomous GNC for the AIM mission

    15'

    confirmed

    Mr. Andrea Pellacani

    G.M.V. Space and Defence, S.A.

    Spain

    3

    Embedded Model Control GNC for the Next Generation Gravity Mission

    15'

    confirmed

    Mr. Luigi Colangelo

    Politecnico di Torino

    Italy

    4

    Development of a Combined Attitude and Position Controller for a Satellite Simulator

    15'

    confirmed

    Mr. Marco Sagliano

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

    Germany

    5

    Integrated 6-DOF spacecraft orbit-attitude dynamics modeling and its application in hovering control over an asteroid

    15'

    withdrawn

    Dr. Yue Wang

    Beihang University

    China

    6

    Far range formation Flight with high risk debris in Low Earth Orbit using relative orbital elements

    15'

    confirmed

    Mr. Mohamed Khalil Ben Larbi

    Technische Universität Braunschweig, Institute of Aerospace Systems

    Germany

    7

    Autonomous Navigation and Guidance for Terminal Maneuver For Docking Using Model Predictive Static Programming (MPSP) and Unscented Kalman Filter (UKF)

    15'

    confirmed

    Mr. RaviKumar L

    ISRO Satellite Centre (ISAC)

    India

    8

    Fractionated Satellite Systems: Station Keeping Strategies

    15'

    confirmed

    Mr. Daniele Filippetto

    Politecnico di Milano

    Italy

    9

    Bounded motions near equilibrium points of contact binary asteroids by a Hamiltonian structure-preserving controller and its applications

    15'

    confirmed

    Dr. Yuying Liang

    China

    10

    Rate Estimation and Damping of a Highly Asymmetrical Tumbling Spacecraft Using Magnetometer Data

    15'

    confirmed

    Ms. shubha kapoor

    Indian Space Research Organization (ISRO)

    India

    11

    reaction-wheels based aocs for high-pointing accuracy and stability

    15'

    confirmed

    Ms. Francesca Cirillo

    Airbus Defence & Space

    Germany

    12

    Magnetometer Only Attitude Estimation for Spin Satellites

    15'

    withdrawn

    Dr. Halil Ersin Soken

    Japan Aerospace Exploration Agency (JAXA), ISAS

    Japan