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  • session 5

    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

    2019-10-23

    Time

    14:45

    Room

    150A

    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;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:45

    SWOT: an AOCS answering to high payload constraints

    15

    confirmed

    Mr. Bertrand RAFFIER

    Centre National d'Etudes Spatiales (CNES)

    France

    2

    15:00

    Impact of Strain-Actuated Attitude Control Systems for Variant Mission Classes

    15

    confirmed

    Mr. FNU Vedant

    University of Illinois

    United States

    3

    15:15

    on the attitude control by thruster of a spinning solar sail and bending moment's effect analysis

    15

    confirmed

    Mr. Roger Bertran Rabat

    Department of Engineering ,The University of Tokyo

    Spain

    4

    15:30

    Semi-analytical Approach to Fasten Complex and Flexible Pointing Strategies Definition for Nanosatellite Clusters: the HERMES Mission Case from Design to Flight

    15

    confirmed

    Mr. Jacopo Prinetto

    Politecnico di Milano

    Italy

    5

    15:45

    Detumbling and Attitude Control of Cubesats via Multi-Model Based Embedded Optimization

    15

    confirmed

    Mr. Wee Meng Ng

    THALES GROUP

    Singapore, Republic of

    6

    16:00

    Model Predictive Steering Control Law for Double-gimbal Scissored Pairs of Control Moment Gyros

    15

    confirmed

    Prof. Hirohisa Kojima

    Tokyo Metropolitan University

    Japan

    7

    16:15

    Control of an Over-Actuated Spacecraft using a Combination of a Fluid Actuator and Reaction Wheels

    15

    confirmed

    Dr. Sebastian Grau

    Technische Universität Berlin

    Germany

    8

    16:30

    Forward Dynamics Algorithm for Origami-Folded Deployable Spacecraft Structures

    15

    confirmed

    Ms. JoAnna Fulton

    University of Colorado Boulder

    United States

    9

    16:45

    Coupled Motion Determination and Stabilization of a Satellite Equipped with Large Flexible Elements Using ADCS Only

    15

    confirmed

    Dr. Danil Ivanov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    10

    17:00

    minimum jerk attitude slew maneuvers

    15

    withdrawn

    Mr. Arland Thompson

    Raytheon

    United States

    11

    17:15

    Design and Hardware-in-the-Loop Test of an Active Magnetic Detumbling and Pointing Control based only on Three-Axis Magnetometer Data

    15

    confirmed

    Mr. Stefano Carletta

    Sapienza University of Rome

    Italy

    12

    17:30

    experimental validation of agile attitude control with sinc function-based profiler for reducing residual vibrations

    15

    confirmed

    Dr. Toshio Kamiya

    NEC Corporation

    Japan