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  • session 3

    Title

    Attitude Dynamics (1)

    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

    2018-10-02

    Time

    14:45

    Room

    CCB Borgward

    IPC members
    • Co-Chair: Prof. Arun Misra, Mc Gill Institute for Aerospace Engineering (MIAE), Canada;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    14:45

    Dynamic Control System Performance of the Space Technology-7 Disturbance Reduction System During the LISA Pathfinder Extended Mission

    15

    withdrawn

    Dr. James O'Donnell

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

    United States

    2

    15:00

    Attitude Control Strategy of a Transformable Spacecraft for Orbital Station-Keeping around Sun-Earth L2

    15

    confirmed

    Mr. Yuki Kubo

    University of Tokyo

    Japan

    3

    15:15

    Solarelastic Stability Modeling and Structural Control of a Heliogyro Solar Sail

    15

    withdrawn

    Dr. Adonis Pimienta-Penalver

    University at Buffalo

    United States

    4

    15:30

    Pure Magnetic Control for Attitude Slew Maneuvers

    15

    confirmed

    Prof. Giulio Avanzini

    Università del Salento

    Italy

    5

    15:45

    Performance characterization of a non-conventional star tracker based on a hyper-hemispherical panoramic camera

    15

    confirmed

    Dr. Roberto Opromolla

    University of Naples "Federico II"

    Italy

    6

    16:00

    time-optimal spacecraft reorientation under multiple constraints via an efficient hybrid optimizer

    15

    confirmed

    Mr. Hui Wang

    Beijing Institute of Technology

    China

    7

    16:15

    On the Smoothing of Slewing Profiles\\ for Low Thrust Transfer Trajectories

    15

    confirmed

    Mr. Pelayo Peñarroya Rodríguez

    OHB System AG-Bremen

    Germany

    8

    16:30

    Cislunar non-Keplerian orbits rendezvous & docking: 6DOF Guidance and Control

    15

    confirmed

    Mr. Andrea Colagrossi

    Politecnico di Milano

    Italy

    9

    16:45

    Tethered towing large space debris with fuel residues by a small spacecraft-tug

    15

    confirmed

    Prof. Vladimir S. Aslanov

    Samara National Research University (Samara University)

    Russian Federation

    10

    17:00

    rigid-flexible coupling dynamics of tethered space debris with solar panels

    15

    confirmed

    Dr. Rui Qi

    Beijing Institute of Technology

    China

    11

    17:15

    Magnetic Detumbling of Fast-tumbling Picosatellites

    15

    confirmed

    Dr. Robert Fonod

    Delft University of Technology

    The Netherlands

    12

    17:30

    Spacecraft Radiation Pressure Using Complex Bidirectional-Reflectance Distribution Functions On Graphics Processing Unit

    15

    withdrawn

    Mr. Patrick Kenneally

    The University of Colorado

    United States