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  • session 4

    Title

    Attitude Dynamics (2)

    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

    2014-10-01

    Time

    09:45

    Room

    801A

    IPC members
    • Co-Chair: Prof.Dr. Kazuya Yoshida, Tohoku University, Japan;

    • Co-Chair: Dr. Simei Ji, Beijing Institute of Technology, China;

    • Rapporteur: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE: Lessons Learned from the Dynamical Behavior of Orbiting Satellites

    30'

    confirmed

    Dr. Jozef van der Ha

    Mission Design & Operations

    United States

    2

    a direct adaptive control law using modified rodrigues parameters for iss attitude regulation during free-flyer capture operations

    15'

    confirmed

    Mr. Jian-Feng Shi

    MDA Corporation

    Canada

    3

    An exponentially fast attitude tracking controller on the rotation group

    15'

    confirmed

    Dr. James Biggs

    University of Strathclyde

    United Kingdom

    4

    active damping algorithm of the international space station structure vibration

    15'

    confirmed

    Mr. Aleksey Zhirnov

    S.P. Korolev Rocket and Space Corporation Energia

    Russian Federation

    5

    A distributed attitude control law for formation flying based on the Cucker-Smale model

    15'

    confirmed

    Mr. Fabrizio Paita

    Universitat Politecnica de Catalunya (UPC)

    Spain

    6

    In Orbit Noise Evaluation of COTS Sensors used for Attitude Determination on AAUSAT3

    15'

    withdrawn

    Mr. Michael Nauheimer

    Aalborg University

    Denmark

    7

    Retraction of the tether on last stag of the deployment procedure for tether-assisted re-entry

    15'

    withdrawn

    Prof. Vladimir S. Aslanov

    Samara National Research University (Samara University)

    Russian Federation

    8

    Robust Nonlinear Control of Underactuated Spacecraft using a Single Thruster

    15'

    confirmed

    Mr. Alexander Frias

    Ryerson University

    Canada

    9

    A Magnetic Control Law for Fast Detumbling of Spacecraft

    15'

    withdrawn

    Mr. Albert Caubet

    University of Strathclyde

    United Kingdom

    10

    attitude determination for small spin satellite based on navigation receiver with single antenna

    15'

    no-show

    Mr. wei wang

    Shanghai Institute of Satellite Engineering

    China

    11

    Attitude Control System of the Eu:CROPIS Mission

    15'

    confirmed

    Mr. Ansgar Heidecker

    German Aerospace Center (DLR)

    Germany

    12

    Development of Total Orbital Real-time Attitude control Simulator for Small Satellites

    15'

    confirmed

    Mr. Takayuki Hosoda

    Mitsubishi Precision Co., Ltd.

    Japan