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  • session 2

    Title

    Attitude Dynamics (2)

    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

    2026-10-06

    Time

    10:15

    Room

    Hall 8

    IPC members
    • Co-Chair: Dr. Feng Jinglang, University of Strathclyde, United Kingdom;

    • Co-Chair: Bang Hyochoong, Korea Advanced Institute of Science and Technology (KAIST), Republic of Korea;

    • Rapporteur: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Three-axis Detumbling of Resource-Constrained Femtosatellites

    15

    confirmed

    Mr. Satyam Bhatti

    University of Glasgow

    United Kingdom

    2

    10:30

    Dynamic Instability of a Spinning Ring Tethered Space System with Shifting Center of Mass

    15

    confirmed

    Mr. Jannes Hühnerbein

    Technical University of Munich (TUM)

    Germany

    3

    10:45

    An Approximate Analytical Approach for Attitude Estimation and Prediction of A Tumbling Target

    15

    confirmed

    Dr. Chuan Ma

    Northwestern Polytechnical University

    China

    4

    11:00

    Experimental Validation of Adaptive Attitude Control Considering Time-Varying Mass Properties on a Satellite Testbed

    15

    confirmed

    Mr. Geongsu Park

    Korea Advanced Institute of Science and Technology (KAIST)

    Republic of Korea

    5

    11:15

    Origami-inspired variable-shape aerobrake for satellite attitude control during descent

    15

    confirmed

    Dr. Dmitry A. Sizov

    Nazarbayev University

    Kazakhstan

    6

    11:30

    A Novel Pumped Fluid Spherical Actuator for Satellite Attitude Control

    15

    confirmed

    Dr. Krishna Kumar

    Toronto Metropolitan University

    Canada

    7

    11:45

    Quintic S-Curve SO(3) Quaternion Guidance for Agile, Zero-Overshoot Slews: On-Orbit Demonstration of the Connecta IoT 6U Nanosatellite

    15

    confirmed

    Dr. Gokhan Ozdogan

    Plan-S Satellite and Space Technologies

    Türkiye

    8

    12:00

    Momentum Unloading for Reaction Wheels via Solar Radiation Pressure: Integrating Sun-Tracking and Hardware Constraints

    15

    confirmed

    Dr. Tetsuya Kusumoto

    Japan Aerospace Exploration Agency (JAXA), ISAS

    Japan

    9

    12:15

    A Multispectral Epoch Method Approach to Attitude Determination

    15

    confirmed

    Dr. Fiona Porter

    University of Strathclyde / Mechanical and Aerospace Engineering

    United Kingdom

    10

    12:30

    Time-Varying Dynamic Modeling and Distributed Prescribed-Time Control for On-Orbit Assembly of Large Space Antenna Array

    15

    confirmed

    Mr. Juliang Yue

    College of Astronautics, Northwestern Polytechnical University

    China