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  • 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.

    Date

    2021-10-29

    Time

    09:45

    Room

    Sheikh Maktoum C

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

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

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    The LISA DFACS: effects of micro-meteoroid impacts in the drag-free mode

    10

    confirmed

    Mr. Michele Pagone

    Politecnico di Torino

    Italy

    2

    09:55

    Visual Servoing for Coordinated Precise Attitude Control in the TOM Small Satellite Formation

    10

    confirmed

    Mr. Julian Scharnagl

    Zentrum für Telematik

    Germany

    3

    10:05

    Attitude Dynamics and Operation Result in Hayabusa2 Capsule Reentry

    10

    confirmed

    Mr. Kent Yoshikawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    10:15

    magnetically controllable attitude trajectory constructed using the particle swarm optimization method

    10

    confirmed

    Ms. Anna Okhitina

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    6

    10:25

    Determination and Mitigation of the Residual Magnetic Dipole Moment of CubeSats for Improved Attitude Stability

    10

    confirmed

    Dr. Abdelmadjid Lassakeur

    Agence Spatiale Algérienne (ASAL)

    Algeria

    7

    10:35

    Development and Analysis of a Pitch Sun Tracking Attitude Mode for the 2U CubeSat ORCASat

    10

    confirmed

    Dr. Zeno Pavanello

    University of Padova, DII / CISAS – “G. Colombo”

    Italy

    8

    10:45

    decentralised anti-windup fault tolerant control design for satellite attitude stabilization

    10

    confirmed

    Mr. Ikechukwu Ofodile

    Univeristy of Tartu

    Estonia

    1005

    10:55

    Real-Time Remaining Useful Life Prediction of Spacecraft Reaction Wheels Using Hybrid Model Based on Artificial Intelligence Techniques

    10

    confirmed

    Dr. Krishna Kumar

    Ryerson University

    Canada

    1009

    11:05

    unwinding and singularity free satellite attitude control using double-gimbal variable-speed control moment gyro and sliding control

    10

    confirmed

    Ms. Gargi Das

    Indian Institute of Technology Kharagpur

    India

    1010

    11:15

    A Fuel-Free and Agile Attitude Maneuver of Spinning Space Membrane Structures Using Electromagnetic Force

    10

    withdrawn

    Mr. Yuki Yamada

    Nagoya University

    Japan

    1011

    11:25

    Integrated Navigation Device for CubeSat Attitude Determination

    10

    withdrawn

    Mr. Thu Vu Trong

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    1012

    11:35

    Attitude control of a nanosatellite using inverse simulation

    10

    confirmed

    Mr. Robert Gordon

    School of Engineering, University of Glasgow

    United Kingdom

    *

    data-driven attitude robust control for microsatellite with an 1-D undeployed mechanism

    Mr. Liming Fan

    School of Astronautics, Beihang University

    China

    *

    satellite attitude control using lorentz force generated by charge at low voltage

    confirmed

    Prof. Manoranjan Sinha

    Indian Institute of Technology Kharagpur

    India