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  • session 2

    Title

    Attitude Dynamics (2)

    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 rigid and flexible bodies, including tethered systems, and in-orbit assembly.

    Date

    2022-09-19

    Time

    10:15

    Room

    S05

    IPC members
    • Co-Chair: Prof. Gianmarco Radice, Singapore, Republic of;

    • Co-Chair: Prof. Toshio Kamiya, Meisei University, Japan;

    • Co-Chair: Bang Hyochoong, Korea Advanced Institute of Science and Technology (KAIST), Korea, Republic of;

    • Rapporteur: Dr. Zhanfeng Meng, China Academy of Space Technology (CAST), China;

    • Rapporteur: Mr. Al Cangahuala, National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Attitude maneuvers of a flexible spacecraft for space debris detection and collision avoidance

    15

    confirmed

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    2

    10:30

    attitude estimation using extended h-infinity particle filter applied to china-brazil earth resource satellite-4

    15

    confirmed

    Prof.Dr. William Silva

    University of Brasilia

    Brazil

    3

    10:45

    Laboratory-Scale Demonstration of a Distributed Magnetorquer Array for the Attitude Control of Large Space Structures

    15

    confirmed

    Mr. Bonar Robb

    University of Glasgow

    United Kingdom

    4

    11:00

    Line-of-sight control using double-gimbal control moment gyroscope for tethered satellite equipped with tether-net for debris capture

    15

    confirmed

    Mr. Haruma Suzuki

    Tokyo Metropolitan University

    Japan

    5

    11:15

    Optimal Actuator-based Attitude Maneuvering of Constrained Spacecraft via Motion Planning Algorithms

    15

    confirmed

    Mr. Riccardo Calaon

    University of Colorado Boulder

    United States

    6

    11:30

    Spacecraft attitude control using PD controller with gain tunning by neuro-fuzzy system.

    15

    Dr. Sung-Woo Kim

    Hanwha Thales

    Korea, Republic of

    7

    11:45

    adcs rate controller using intermediate axis theorem

    15

    confirmed

    Mr. Sander Kvalsvik

    Norwegian University of Science and Technology

    Norway

    8

    12:00

    Dynamics and Stability Analysis of Spacecraft Attitude Considering High-Fidelity Solar Radiation Pressure

    15

    confirmed

    Mr. Masaki Kakeru

    Kyushu University

    Japan

    9

    12:15

    Application of deep reinforcement learning for attitude control of a satellite in the presence of uncertainties

    15

    confirmed

    Mr. Jan Loettgen

    School of Engineering, University of Glasgow

    United Kingdom

    10

    12:30

    Choice of design parameters of a CubeSat 6U for providing three-axis passive stabilization

    15

    confirmed

    Prof. Igor V. Belokonov

    Samara National Research University (Samara University)

    Russian Federation