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  • session 6

    Title

    Attitude Dynamics (2)

    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

    2015-10-15

    Time

    09:45

    Room

    Teddy B (ICC, lower level)

    IPC members
    • Co-Chair: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;

    • Co-Chair: Prof. Yong Chun Xie, Beijing Institute of Control Engineering, China Academy of Space Technology (CAST), China;

    • Rapporteur: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    Absolute Attitude Determination System for a Spherical Air Bearing Testbed

    16'

    confirmed

    Dr. Jason Forshaw

    Surrey Space Centre, University of Surrey

    United Kingdom

    2

    10:01

    attitude control of an aggregated modular spacecraft with momentum reaction sphere actuators

    16'

    withdrawn

    Dr. Chunshi FAN

    China Academy of Space Technology (CAST)

    China

    3

    10:17

    Equilibrium configurations for attitude and orbital control by tether system.

    16'

    no-show

    Dr. Denilson Paulo Souza dos Santos

    Instituto Nacional de Pesquisas Espaciais - INPE (Brasil) \ Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal

    Brazil

    4

    10:33

    Modeling and Dynamics of Variable Mass Tethered System with Chemical Propulsion

    16'

    confirmed

    Dr. Liang Sun

    Beihang University

    China

    5

    10:49

    Analysis and experiments for a system of two spacecraft paired by means of a flexible link

    16'

    confirmed

    Dr. Marco Sabatini

    Sapienza University of Rome

    Italy

    6

    11:05

    Chaotic behavior of a passive satellite during towing by a tether

    16'

    confirmed

    Prof. Vladimir S. Aslanov

    Samara State Aerospace University

    Russian Federation

    7

    11:21

    Research on Novel Integrated Rudder Actuation System for Spacecraft Reentry Aerodynamic Control Based on Double Digital Closed Channels of Power Management and Load Damping

    16'

    withdrawn

    Dr. yuexuan wang

    China Academy of Launch Vehicle Technology (CALT)

    China

    8

    11:37

    An Angular Momentum Ring Storage Device Prototype for Cubesats based on a Liquid Metal Actuator

    16'

    confirmed

    Mr. Sebastian Grau

    Technische Universität Berlin

    Germany

    9

    11:53

    Dynamic Modeling and Control Simulation of the Cabin Transferring Assisted by Manipulator for the China Space Station

    16'

    confirmed

    Dr. Dongming Ge

    China Academy of Space Technology (CAST)

    China

    10

    12:09

    Spacecraft Attitude and Total Power Optimal Control with Redundant Double-Gimbal Variable-Speed Control Moment Gyros

    16'

    confirmed

    Mr. Takahiro Sasaki

    Osaka Prefecture University

    Japan

    11

    12:25

    Link loss recovery strategy using sun sensor and beacon signal in Mars orbiter Mission

    16'

    confirmed

    Ms. Ritu Karidhal

    ISRO Satellite Centre (ISAC)

    India