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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

    2017-09-25

    Time

    15:15

    Room

    Hall A

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

    • Co-Chair: Dr. James O'Donnell, National Aeronautics and Space Administration (NASA), Goddard Space Flight Center, United States;

    • Rapporteur: Prof. Gianmarco Radice, University of Glasgow, United Kingdom;

    papers

    Order

    Presentation status

    Mode

    Paper title

    Main author

    Affiliation

    Country

    1

    confirmed

    coulomb tether double-pyramid satellite formations: with application to GEO satellite collocation

    Mr. Anrui Shi

    Beijing Institute of Technology

    China

    2

    confirmed

    Force and Torque Disturbance Modeling Due to General Thruster Plume Impingements

    Mr. Thibaud Teil

    University of Colorado Boulder

    United States

    3

    confirmed

    Time-Varying Errors for Magnetometers on Small Satellites

    Dr. Halil Ersin Soken

    Japan Aerospace Exploration Agency (JAXA), ISAS

    Japan

    4

    confirmed

    Dynamic Control System Mode Performance of the Space Technology-7 Disturbance Reduction System

    Dr. James O'Donnell

    National Aeronautics and Space Administration (NASA), Goddard Space Flight Center

    United States

    5

    confirmed

    Attitude Stabilization of a Flexible Spacecraft using combined PZT/optical sensors

    Dr. Marco Sabatini

    Università di Roma "La Sapienza"

    Italy

    6

    confirmed

    magnetic attitude control of satellites using coarse pulse-width-modulation of magnetorquers

    Dr. Yasuhiro Yoshimura

    Tokyo Metropolitan University

    Japan

    7

    withdrawn

    L1 adaptive control of spacecraft flying in very Low Earth Orbits using aerodynamic torques

    Mr. Zhou Hao

    The University of Manchester

    United Kingdom

    8

    confirmed

    Investigation into Integrated Attitude Determination in High-Precision CubeSats

    Mr. Joshua Critchley-Marrows

    The University of Sydney

    Australia

    9

    confirmed

    Multifunctional Optical Attitude Determination Sensor for Picosatellites

    Mr. Nikolas Korn

    Technische Universität Berlin

    Germany

    10

    withdrawn

    Tether deployment using high spin rate control for interplanetary nanosatellite missions

    Mr. Ikechukwu Ofodile

    Univeristy of Tartu

    Estonia

    11

    confirmed

    Fully-Coupled Dynamical Jitter Modeling of a Rigid Spacecraft with Imbalanced Double-Gimbal Variable-Speed Control Moment Gyros

    Mr. Takahiro Sasaki

    Colorado Center for Astrodynamics Research, University of Colorado

    United States

    12

    confirmed

    High dynamic star tracker for remote sensing satellite

    Dr. Ting Sun

    Tsinghua University

    China