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    Attitude Dynamics (1)


    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: Dr. Shinji Hokamoto, Kyushu University, Japan;

    • Co-Chair: Prof. Gianmarco Radice, Singapore, Republic of;

    • Rapporteur: Prof. Giovanni B. Palmerini, Sapienza University of Rome, Italy;