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  • session 8

    Title

    Attitude Dynamics (1)

    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

    09:00

    Room

    TS01 (Sala Aldebaran, Hall 1)

    IPC members
    • Chairman: Prof. Gianmarco Radice, Singapore, Republic of;

    • Chairman: Prof.Dr. Kazuya Yoshida, Tohoku University, Japan;

    • Rapporteur: Dr. Simei Ji, Beijing Institute of Technology, China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    COUPLED ORBIT AND ATTITUDE DYNAMICS FOR A SPACECRAFT COMPRISED OF MULTIPLE BODIES IN EARTH-MOON HALO ORBITS

    15'

    confirmed

    Ms. Amanda Knutson

    Purdue University

    United States

    2

    AOCS science mode design for ESA’s EUCLID mission

    15'

    withdrawn

    Mr. Alberto Anselmi

    Thales Alenia Space Italia

    Italy

    3

    Zero-propellant attitude maneuver path planning of space station based on simple gimbal control moment gyroscopes

    15'

    confirmed

    Dr. Hai-bing Huang

    National University of Defense Technology

    China

    4

    Robustness Analyses of Attitude Slew Manoeuvres for Spinning Penetrator Spacecraft

    15'

    confirmed

    Mr. Robin Raus

    EADS Astrium

    United Kingdom

    5

    REX-J (Robot Experiment on ISS/JEM) to demonstrate astronaut support robot - Result of the in-orbit check out of the REX-J mission

    15'

    confirmed

    Prof.Dr. Mitsushige Oda

    JAXA

    Japan

    6

    Development of sun-pointing magnetic attitude control system for cxbn cubesat

    15'

    confirmed

    Mr. Paride Testani

    Scuola Ingegneria Aerospaziale

    Italy

    7

    Dynamic Modelling and Control of Flexible Robotic Space Manipulators with Telescoping Booms

    15'

    confirmed

    Mr. Alex Walsh

    McGill University

    Canada

    8

    First in-orbit results of the Pleiades CMG-based attitude control system

    15'

    confirmed

    Dr. Charles Koeck

    EADS Astrium

    France

    9

    Space manipulator control for the DYMAFLEX flight experiment

    15'

    confirmed

    Mr. Nicholas D'Amore

    University of Maryland, College Park

    United States

    10

    Investigation of On-Orbit Electodynamic Tether Deployment by Ground Experiment and Numerical Simulation using a Detailed Friction Model

    15'

    confirmed

    Mr. Mitsuhisa Baba

    Waseda University

    Japan

    11

    Experimental orbital rendezvous operations via visual based techniques

    15'

    confirmed

    Dr. Marco Sabatini

    Sapienza University of Rome

    Italy

    12

    Path planning of experimental module transfer for minimizing attitude disturbance of space station

    15'

    withdrawn

    Mr. Yi Wang

    National University of Defense Technology

    China

    13

    A Sensitivity Analysis Approach in the Design of the Attitude Control System of Small Satellites

    15'

    confirmed

    Prof. Teodor-Viorel Chelaru

    University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space

    Romania