• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-10
  • C1
  • 4
  • session 4

    Title

    Attitude Dynamics (2)

    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

    2010-09-29

    Time

    10:15

    Room

    North Hall

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

    • Chairman: Prof. Gerard Gomez, University of Barcelona, Spain;

    • Rapporteur: Prof. Weihua Zhang, National University of Defense Technology, China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    CMG gimbal angles planner based on Rapidly-exploring Random Trees algorithms

    15

    withdrawn

    Mr. Marco Anania

    Thales Alenia Space Italia

    Italy

    2

    Design and validation of geometric optimisation software for the attitude control of microsatellites

    15

    confirmed

    Dr. Nadjim Mehdi Horri

    Surrey Space Centre, University of Surrey

    United Kingdom

    3

    Attitude Control of IKAROS Solar Sail Spacecraft and Its Flight Results

    15

    confirmed

    Prof. Ryu Funase

    University of Tokyo

    Japan

    4

    Reconfigurable Cooperative Attitude Control of Magnetically Actuated Satellites Formation

    15

    withdrawn

    Dr. Manoranjan Sinha

    Indian Institute of Technology

    India

    5

    Fault Detection and Fault Tolerant Control for AAUSAT3 Cubesat

    15

    Mr. Bjørn Eskildsen

    Aalborg University

    Denmark

    6

    Nonlinear fault tolerant attitude control for FAST-D spacecraftr

    15

    withdrawn

    Dr. Q.P. Chu

    Delft University of Technology (TU Delft)

    The Netherlands

    7

    a space mobile robot using tethered moving methods. – study of tether's location and robot's locomotion capability -

    15

    confirmed

    Mr. Mitsuhiro Yamazumi

    Tokyo Institute of Technology

    Japan

    8

    Mission-oriented Micro-Sun-Sensor Laboratory Testing in Real-Time Operation Mode

    15

    confirmed

    Prof. Michele Grassi

    University of Naples "Federico II"

    Italy

    9

    An attitude model for the spacecraft of the ESA mission Gaia

    15

    confirmed

    Dr. Ralf Keil

    ZARM University of Bremen

    Germany

    10

    Research on the pointing control computation and realization method of TDRS tracking the LEO spacecraft

    15

    withdrawn

    Dr. wu gang

    Beijing Institute of Tracking and Telecommunication Technology (BITTT)

    China

    11

    Nonlinear Estimation for Vision-based Target Attitude Measurement in Space Operation

    15

    confirmed

    Mr. Haifeng Su

    College of Astronautics, Northwestern Polytechnical University

    China

    12

    Three-axis Stabilization of a Low Earth Orbit Spacecraft utilizing Three Magnetorquers and Reaction Wheels Combinations, according to Energy Consumption

    15

    confirmed

    Prof. M. Navabi

    Shahid Beheshti University

    Iran