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  • session 3

    Title

    Attitude Dynamics (1)

    type

    oral

    Description

    This theme discusses advances in spacecraft attitude dynamics and control, as well as design, testing and performance of novel attitude sensors and actuators. This theme also covers dynamics and control of multiple interconnected regidi and flexible bodies, including tethered systems, an in-orbit assembly.

    Date

    2014-09-30

    Time

    14:45

    Room

    801A

    IPC members
    • Co-Chair: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;

    • Co-Chair: Mrs. Amalia Ercoli Finzi, Politecnico di Milano, Italy;

    • Rapporteur: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    new one-axis magnetic attitude control in absence of magnetometer readings

    15'

    confirmed

    Dr. Stepan Tkachev

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    2

    autonomous spacecraft attitude constraints avoidance

    15'

    confirmed

    Mr. Ofer Salama

    Rafael Advanced Defense Systems Ltd.

    Israel

    3

    An Angular Momentum Ring Storage Device for Small Satellites Based on a Liquid Metal Actuator

    15'

    confirmed

    Mr. Daniel Noack

    Technische Universität Berlin

    Germany

    4

    Attitude Control of Large Gossamer Spacecraft using Surface Reflectivity Modulation

    15'

    confirmed

    Mr. Andreas Borggräfe

    University of Strathclyde

    United Kingdom

    5

    THRUSTER FAULT DETECTION ISOLATION AND RECONFIGURATION FOR INDIAN MARS ORBITER

    15'

    confirmed

    Ms. shubha kapoor

    Indian Space Research Organization (ISRO)

    India

    6

    Practical consideration of spacecraft attitude and rate determination using numerical Gyros

    15'

    confirmed

    Dr. Hao-Chi Chang

    National Space Organization

    Taiwan, China

    7

    BepiColombo: Dynamics analysis following module separation

    15'

    confirmed

    Mr. Frederik Belien

    Airbus Defense and Space

    Germany

    9

    Dynamic analysis of thin-film solar panels in LEO

    15'

    confirmed

    Ms. Laura Bettiol

    University of Padova - DII

    Italy

    13

    Robust Backstepping Control of Magnetically Actuated Satellites with Unsymmetrical Mass Properties

    15'

    confirmed

    Mr. Dipak Kumar Giri

    Indian Institute of Technology

    India