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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

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

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

    15'

    confirmed

    Dr. Rui Zhong

    York University

    China

    2

    10:00

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

    15'

    confirmed

    Dr. yuexuan wang

    China Academy of Launch Vehicle Technology (CALT)

    China

    3

    10:15

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

    15'

    confirmed

    Mr. Lawrence Inumoh

    Surrey Space Centre, University of Surrey

    United Kingdom

    4

    10:30

    A residual-based Adaptive Unscented Kalman Filter for microsatellites

    15'

    confirmed

    Dr. Le Xuan Huy

    Tokyo Institute of Technology

    Vietnam

    5

    10:45

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

    15'

    confirmed

    Dr. Marco Sabatini

    Sapienza University of Rome

    Italy

    6

    11:00

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

    15'

    confirmed

    Dr. Shunan Wu

    Dalian University of Technology

    China

    7

    11:15

    Determination of spacecraft inertial parameters on board.

    15'

    withdrawn

    Mr. Dmitry Timoshin

    TSNIIMASH

    Russian Federation

    8

    11:30

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

    15'

    confirmed

    Mr. Saroj Kumar

    Nitte Meenakshi Institute Of Technology.

    India

    9

    11:45

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

    15'

    confirmed

    Mr. Mingming Wang

    Technical University of Munich

    Germany

    10

    12:00

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

    15'

    confirmed

    Dr. Mohammad Abdelrahman

    International Islamic University Malaysia

    Malaysia

    11

    12:15

    Control algorithms development for space platform with a rotating solar sail

    15'

    confirmed

    Mr. Aleksandr Zykov

    S.P. Korolev Rocket and Space Corporation Energia

    Russian Federation

    12

    12:30

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

    15'

    confirmed

    Dr. Wei Zhang

    China Aerospace Science and Industry Corporation

    China

    13

    12:45

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

    15'

    confirmed

    Mr. Aidin Mohammadi

    Aerospace Research Institute

    Iran