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  • session 9

    Title

    Attitude Dynamics (2)

    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: Prof. Gianmarco Radice, Singapore, Republic of;

    • Co-Chair: Dr. Toshio Kamiya, NEC Corporation, Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    attitude control of satellites with variable shape function utilizing atmospheric drag torque and magnetic torque

    15

    confirmed

    Mrs. Kiyona Miyamoto

    Tokyo Institute of Technology

    Japan

    2

    three-dimensional attitude control of spacecraft by three thrusters

    15

    confirmed

    Dr. Shinji Hokamoto

    Kyushu University

    Japan

    3

    Attitude dynamics and integrated robust control of the multi-rotary joints solar power satellite

    15

    withdrawn

    Dr. Shunan Wu

    Dalian University of Technology

    China

    4

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

    15

    withdrawn

    Dr. Abdelmadjid Lassakeur

    Agence Spatiale Algérienne (ASAL)

    Algeria

    5

    The LISA DFACS: preliminary Model Predictive Control design for the test mass release phase

    15

    confirmed

    Dr. Simone Vidano

    Politecnico di Torino

    Italy

    6

    Dark Universe Euclid mission: Highest pointing and stability AOCS, performance achievement and verification

    15

    Mr. Salvador Llorente-Martínez

    SENER

    Spain

    7

    Attitude Control Algorithms Aided by Multipoint Statistics and Distributed Measurements Processing in a Swarm of CubeSats

    15

    confirmed

    Mr. Anton Afanasev

    Skolkovo Institute of Science and Technology

    Russian Federation

    8

    Autonomous Spacecraft Attitude Control Using Deep Reinforcement Learning

    15

    confirmed

    Mr. Jacob Elkins

    The University of Alabama

    United States

    9

    An Energy-Based Approach to Satellite Attitude Control in Presence of Disturbances for a CubeSat Mission

    15

    confirmed

    Mr. Adolfo Chaves Jiménez

    Instituto Tecnológico de Costa Rica (TEC)

    Costa Rica

    10

    imaging-based attitude determination algorithm for small satellites: design and the preliminary results

    15

    confirmed

    Mr. Mehmet Burak Güzel

    Middle East Technical University

    Turkey

    11

    Design of suboptimal turn-time algorithm for 3-axial attitude maneuvering

    15

    Mr. Nikita Ivlev

    Moscow Institute of Physics and Technology (MIPT)

    Russian Federation

    12

    Reaction Wheel Failure Attenuation For Nano-spacecrafts In Low Earth Orbits

    15

    Mr. Ahmed Mahfouz

    Skolkovo Institute of Science and Technology

    Russian Federation

    13

    Adaptive Control Based on Disturbance Observer for Non-cooperative Spacecraft Proximity Operations Using T-S Fuzzy Approach

    Ms. Na Wu

    China

    14

    Problems of Development of an Experimental Platform “the Angular Orientation and Stabilization Stand”

    confirmed

    Mr. Bohdan Bukaiev

    Oles Honchar Dnipropetrovsk National University

    Ukraine

    15

    Improving the attitude determination sensors and algorithms for a CubeSat - ESTCube-2 example

    Mr. Hendrik Ehrpais

    University of Tartu

    Estonia