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  • session 1

    Title

    Attitude Dynamics (1)

    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

    2023-10-03

    Time

    15:00

    Room

    BCC B4

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

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

    • Rapporteur: Prof. Robert G. Melton, Pennsylvania State University, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Absolute Visual Servoing for Precise Earth Target Pointing Onboard Small Satellites

    15

    confirmed

    Mr. Ilham Mammadov

    Zentrum für Telematik

    Germany

    2

    15:15

    Pointing Stability of HiZ-GUNDAM Satellite After Agile Attitude Maneuvers Under the Rate Bias Error of Fiber Optic Gyros

    15

    confirmed

    Prof. Toshio Kamiya

    Meisei University

    Japan

    3

    15:30

    Deep reinforcement learning-based gain scheduling for attitude control of microsatellites with changing inertia

    15

    withdrawn

    Mr. Joe Gibbs

    School of Engineering, University of Glasgow

    United Kingdom

    4

    15:45

    Optimal Attitude Path Planning Along Torque Equilibrium Points Using Aerodynamic Database for Deorbiting Large Debris by Small Satellites

    15

    confirmed

    Dr. Takahiro Sasaki

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    5

    16:00

    Multi-objective Optimization of Attitude Maneuver Planning for Flexible Asteroid Lander Using Population Evolutionary Algorithm

    15

    Mr. Zhe Zhu

    Beijing Institute of Technology

    China

    6

    16:15

    The effects of pointing error sources on energy delivery from orbiting solar reflectors

    15

    confirmed

    Dr. Iain Moore

    University of Glasgow

    United Kingdom

    7

    16:30

    A Free-Floating 3-axis Attitude Control Test Environment with Optical Tracking for High-Precision Pointing Verification of CubeSats

    15

    confirmed

    Mr. Ilham Mammadov

    Zentrum für Telematik

    Germany

    8

    16:45

    Liquid-filled spacecraft finite-time attitude maneuver control with angular and velocity constraint

    15

    confirmed

    Ms. Wei Zhang

    School of Astronautics, Harbin Institute of Technology

    China

    9

    17:00

    Attitude Dynamics of Small Satellites in Circular Near-Equatorial LEO/VLEO

    15

    confirmed

    Dr. Dmitry A. Sizov

    Nazarbayev University

    Kazakhstan

    10

    17:15

    Prescribed Performance Adaptive Control with Fault-tolerance Capability for a Sun-pointing Spacecraft on Halo Orbit

    15

    confirmed

    Mr. Srianish Vutukuri

    Indian Institute of Science

    India