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  • session 9

    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

    2016-09-30

    Time

    13:30

    Room

    Salon Jalisco E6

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

    • Co-Chair: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;

    • Rapporteur: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Periodic orbit-attitude solutions along planar orbits in a perturbed circular restricted three-body problem for the Earth-Moon system

    15'

    confirmed

    Mr. Lorenzo Bucci

    Politecnico di Milano

    Italy

    2

    Orbit-attitude Coupled Motion around Small Bodies: Sun-synchronous Orbits with Sun-tracking Attitude Motion

    15'

    confirmed

    Mr. Shota Kikuchi

    University of Tokyo

    Japan

    4

    Capturing and Docking Spacecraft with Flux Pinned Interfaces

    15'

    confirmed

    Ms. Frances Zhu

    Cornell University

    United States

    5

    Star Tracker Performance during the Early Phases of the Lisa Pathfinder Mission

    15'

    confirmed

    Dr. Jonathan Grzymisch

    European Space Agency (ESA-ESTEC)

    The Netherlands

    6

    Fractional PID Control of Spacecraft Attitude Dynamics using Rotation Matrices

    15'

    confirmed

    Prof. Eric Butcher

    University of Arizona

    United States

    7

    Gain-Scheduled Attitude Control with Power Tracking and Singularity Avoidance of Double-Gimbal Variable-Speed Control Moment Gyros

    15'

    confirmed

    Mr. Takahiro Sasaki

    Osaka Prefecture University

    Japan

    8

    Operations in space of SPACESTAR: the new star tracker for future recurrent platforms

    15'

    confirmed

    Mr. FRANCO BOLDRINI

    Leonardo S.p.A

    Italy

    11

    Dual tensor solution to the extended Wahba problem

    15'

    confirmed

    Prof. Daniel Condurache

    Technical University of Iasi

    Romania

    13

    Motion Prediction of Non-Cooperative Target Based on Autoregressive Model

    15'

    confirmed

    Dr. Mingming Wang

    Northwestern Polytechnical University

    China