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  • 8
  • session 8

    Title

    Attitude Dynamics (1)

    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.

    IPC members
    • Co-Chair: Dr. Shinji Hokamoto, Kyushu University, Japan;

    • Co-Chair: Prof. Giovanni B. Palmerini, Sapienza University of Rome, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Rao-Blackwellized particle filter for the CBERS-4 attitude and gyros bias estimation

    10

    confirmed

    Prof.Dr. William Silva

    University of Brasilia

    Brazil

    2

    Adaptive Torque Equilibrium Attitude Guidance for Rapid Deorbit of Space Debris by Aerodynamic Drag Considering Model Uncertainty

    10

    confirmed

    Dr. Takahiro Sasaki

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    Attitude dynamics and control of space object during contactless transportation by ion beam

    10

    confirmed

    Prof. Vladimir S. Aslanov

    Moscow Aviation Institute

    Russian Federation

    5

    Fuzzy Logic attitude controller implementation on board OPS-SAT

    10

    confirmed

    Mr. Karl Stephan Olfe García

    E-USOC, Universidad Politécnica de Madrid

    Spain

    6

    From Magnetic to Aerodynamic Passive Stabilization: Case of Transient Attitude Motion of TNS-0#2 Nanosatellite

    10

    confirmed

    Dr. Danil Ivanov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    8

    Initial Study on Attitude Control of transformable Spacecraft around Unstable Equilibrium Point Using Solar Radiation Pressure

    10

    confirmed

    Mr. Yudai Kimishima

    Aoyama Gakuin University

    Japan

    9

    CMG Based Steering for Enhancing Agility of High Throughput Satellites

    10

    confirmed

    Mr. ASHOK KUMAR K

    U R RAO SATELLITE CENTRE (URSC)

    India

    12

    Attitude determination and control system for the first SAR satellite in a constellation of iQPS

    10

    confirmed

    Dr. Dmytro Faizullin

    Institute for Q-shu Pioneer of Space, Inc. (iQPS)

    Japan

    13

    Drag-Based Orbit Phasing Through Attitude and Articulation Control

    10

    confirmed

    Mr. Robert Magner

    Space Flight Laboratory, University of Toronto

    Canada

    14

    real-time magnetometer calibration using a three-axis helmholtz coil

    10

    confirmed

    Dr. Amir Labibian

    Satellite Research Institute, Iranian Space Research Center

    Iran