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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 attitude sensors and actuators. The theme also covers dynamics and control of multiple interconnected rigid and flexible bodies including tethered systems and space robots.

    Date

    2012-10-05

    Time

    14:00

    Room

    TS01 (Sala Aldebaran, Hall 1)

    IPC members
    • Chairman: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;

    • Chairman: Bang Hyochoong, Korea Advanced Institute of Science and Technology (KAIST), Korea, Republic of;

    • Rapporteur: Mrs. Amalia Ercoli Finzi, Politecnico di Milano, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Neural-Network-Based Wide-FOV CMOS Sun Sensor

    15'

    confirmed

    Prof. Michele Grassi

    University of Naples "Federico II"

    Italy

    2

    Practical approach for quick attitude maneuver of spacecraft with actuator saturation

    15'

    confirmed

    Mr. Hyosang Yoon

    Satrec Initiative

    Korea, Republic of

    3

    SDS-4 Attitude Control System: First Flight Results of Attitude Control Response

    15'

    confirmed

    Mr. Yuta Nakajima

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    Dynamics of a tether connected to an Irregular Shaped Celestial Body

    15'

    confirmed

    Mr. Mohammad J. Mashayekhi

    McGill University

    Canada

    5

    RACS QFR Algorithm for VEGA FPSA Program

    15'

    confirmed

    Mr. Giovanni Cuciniello

    CIRA Italian Aerospace Research Centre

    Italy

    6

    Dual Attitude and Parameter Estimation of Passively Magnetically Stabilized Spacecraft

    15'

    confirmed

    Mr. Roland Burton

    Stanford University

    United States

    7

    Attitude motion planning for a spin stabilised disk sail

    15'

    confirmed

    Mr. Craig Maclean

    Advanced Space Concept Laboratory, University of Strathclyde

    United Kingdom

    8

    Controllability of Propellant-free Attitude Control System for Spinning Solar Sail Using Thin-Film Reflectivity Control Devices Considering Arbitrary Sail Deformation

    15'

    confirmed

    Prof. Ryu Funase

    University of Tokyo

    Japan

    9

    Coupled Orbital and Attitude Control of Spacecraft in Formation

    15'

    withdrawn

    Mr. Mattia Zamaro

    Politecnico di Milano

    United Kingdom

    10

    Coupled Orbit and Attitude Dynamics of a Reconfigurable Spacecraft with Solar Radiation Pressure

    15'

    confirmed

    Mr. Andreas Borggräfe

    University of Strathclyde

    United Kingdom

    11

    Attitude Determination Of About One Degree accuracy Using only Magnetometer Data In Megha-Tropiques

    15'

    confirmed

    Mr. Nitin Ghatpande

    Indian Space Research Organization (ISRO)

    India

    12

    Development, complex investigation, laboratory and flight testing of the magneto-gyroscopic ACS for the microsatellite

    15'

    confirmed

    Prof. Michael Yu Ovchinnikov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    13

    Optimal Attitude Maneuver Path Planning for Spacecraft under Complex Geometry Constraints

    15'

    confirmed

    Dr. Qian Zhao

    National University of Defense Technology

    China