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  • session 2

    Title

    Attitude Dynamics (2)

    Description

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

    Date

    2013-09-24

    Time

    09:45

    Room

    306A

    IPC members
    • Chairman: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;

    • Chairman: Prof. Hyochoong Bang, Korea Advanced Institute of Science and Technology (KAIST), Korea, Republic of;

    • Rapporteur: Mrs. Amalia Ercoli Finzi, Politecnico di Milano, Italy;

    papers

    Order

    Presentation status

    Mode

    Paper title

    Speaker

    Affiliation

    Country

    1

    confirmed

    15'

    LONG TERM DYNAMICS AND CONTROL OF A BARE ELECTRODYNAMIC TETHERS UNDER MULTI-ENVIRONMENT PERTURBATIONS

    Dr. Rui Zhong

    York University

    China

    2

    confirmed

    15'

    Research on Design and Performance Analysis of High Power Electromechanical Actuator Applied to Spacecrafts

    Dr. yuexuan wang

    China Academy of Launch Vehicle Technology (CALT)

    China

    3

    confirmed

    15'

    experimental demonstration of 3-dof capabilities of a tilted wheel using an air-bearing table

    Mr. Lawrence Inumoh

    Surrey Space Centre, University of Surrey

    United Kingdom

    4

    confirmed

    15'

    A residual-based Adaptive Unscented Kalman Filter for microsatellites

    Dr. Le Xuan Huy

    Tokyo Institute of Technology

    Vietnam

    5

    confirmed

    15'

    ANALYSIS AND EXPERIMENTS FOR DELAY COMPENSATION IN ATTITUDE CONTROL OF FLEXIBLE SPACECRAFT

    Dr. Marco Sabatini

    Sapienza University of Rome

    Italy

    6

    confirmed

    15'

    observer-based robust sliding mode control for spacecraft attitude maneuver subject to reaction wheel friction

    Dr. Shunan Wu

    Dalian University of Technology

    China

    7

    withdrawn

    15'

    Determination of spacecraft inertial parameters on board.

    Mr. Dmitry Timoshin

    TSNIIMASH

    Russian Federation

    8

    confirmed

    15'

    two stage de-tumbling for twin nano-satellites studsat-2a/2b

    Mr. Saroj Kumar

    Nitte Meenakshi Institute Of Technology.

    India

    9

    confirmed

    15'

    Joint-Space Dynamics Algorithm of Space Manipulators with Tree Structure by Using Inertia Mapping Matrix

    Mr. Mingming Wang

    Technical University of Munich

    Germany

    10

    confirmed

    15'

    Spacecraft Sun Pointing Using Coplanar Solar Panels Data and Magnetic Field Measurements

    Dr. Mohammad Abdelrahman

    International Islamic University Malaysia

    Malaysia

    11

    confirmed

    15'

    Control algorithms development for space platform with a rotating solar sail

    Mr. Aleksandr Zykov

    S.P. Korolev Rocket and Space Corporation Energia

    Russian Federation

    12

    confirmed

    15'

    a method of guide star selection for star identification in the condition of high background and high dynamic

    Dr. Wei Zhang

    China Aerospace Science and Industry Corporation

    China

    13

    confirmed

    15'

    robust sliding mode control of a moving-mass actuated suborbital reentry biological payload

    Mr. Aidin Mohammadi

    Aerospace Research Institute

    Iran