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  • session 1

    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.

    Date

    2024-10-16

    Time

    15:00

    Room

    Blue Hall 2

    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

    Attitude Control in Wheel Reduction Operation of Hayabusa2 Extended Mission

    15

    confirmed

    Mr. Takefumi Kosaka

    NEC Corporation

    Japan

    2

    15:15

    Spacecraft Attitude Control in Low-Earth Orbit in the Presence of Slosh

    15

    withdrawn

    Dr. William Elke

    National Aeronautics and Space Administration (NASA), Langley Research Center

    United States

    3

    15:30

    Gravity gradient effects on the attitude dynamics on satellites in Near-Rectilinear Halo Orbits

    15

    confirmed

    Dr. Erica Scantamburlo

    Politecnico di Torino

    Italy

    4

    15:45

    Real-time attitude control for optimal low-thrust multi-revolution coplanar transfers

    15

    confirmed

    Dr. Stefano Carletta

    Sapienza University of Rome

    Italy

    5

    16:00

    Agile attitude control of variable-shape spacecraft with reduced time delay

    15

    confirmed

    Dr. Kei Watanabe

    Tokyo Institute of Technology

    Japan

    6

    16:15

    Study of attitude determination accuracy and Earth-point stabilization performance using asynchronous star tracker and angular velocity sensor measurements

    15

    confirmed

    Dr. Danil Ivanov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    7

    16:30

    Analysis method and research of contact collision process based on attitude evolution of fast tumbling target in space

    15

    confirmed

    Ms. Jiale Chen

    Northwestern Polytechnical University;National Key Laboratory of Aerospace Flight Dynamics

    China

    8

    16:45

    A causal learning approach to in-orbit inertial parameter estimation for multi-payload deployers.

    15

    confirmed

    Mr. Konstantinos Platanitis

    Cranfield University, UK

    United Kingdom

    9

    17:00

    GYSELE : an attitude estimation and non-stellar object tracking system

    15

    confirmed

    Mr. Etienne Perot

    Centre National d'Etudes Spatiales (CNES)

    France

    10

    17:15

    Control of external directional exposures of various surface locations on the tumbling spacecraft using "Inertial Morphing"

    15

    confirmed

    Prof. Pavel M. Trivailo

    RMIT University, Australia

    Australia

    1*

    15:00

    Model Predictive Control for underactuated spacecraft equipped with two reaction wheels in the presence of a residual angular momentum

    15

    confirmed

    Prof. Giulio Avanzini

    Università del Salento

    Italy

    2*

    15:15

    Autonomous Fault Management in Attitude Determination and Control Subsystems: Hardware and Processor in the Loop Testing

    15

    confirmed

    Dr. Andrea Colagrossi

    Politecnico di Milano

    Italy

    3*

    15:30

    Optimization of Electrospray Thruster Configuration and Control Allocation for Spacecraft Attitude Control

    15

    confirmed

    Mr. Riccardo Gatti

    Politecnico di Torino

    Italy

    4*

    15:45

    Deep learning based resolution of attitude ambiguities for relative pose estimation of unknown and uncooperative targets

    15

    confirmed

    Mr. Matteo Rosa

    Politecnico di Milano

    Italy

    5*

    16:00

    adaptive correction network incorporating rate gyro weighting for heavy launch vehicle attitude control

    15

    confirmed

    Mr. Xing-yu Jiang

    Beihang University (BUAA)

    China