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  • session 3

    Title

    Space Structures - Dynamics and Microdynamics

    Description

    Topics included in this session are: Dynamics analysis and testing, modal identification, landing and impact dynamics, pyroshock, test facilities, vibration suppression techniques, damping, micro-dynamics, in-orbit dynamic environment, wave structural propagation, excitation sources and in-orbit dynamic testing.

    Date

    2008-09-30

    Time

    15:00

    Room

    Dochart 1

    IPC members
    • Chairman: Dr. Peter M. Bainum, Howard University, United States;

    • Chairman: Prof. Ijar Da Fonseca, ITA-DCTA, Brazil;

    • Rapporteur: Prof. Harijono Djojodihardjo, Bandung Institut of Tecnology, Indonesia;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Flexibility effects in controlled behaviour of space manipulators

    presentation

    Dr. Chiara Toglia

    University of Rome “La Sapienza”

    Italy

    2

    Interactive Virtual Reality Simulator for the Optimally Controlled Space Robotic Manipulators

    presentation

    Prof. Pavel M. Trivailo

    RMIT University, Australia

    Australia

    3

    Coupled Dynamic Load Analsyis with Different Component Damping of the Substructures

    presentation

    Dr. Andreas Rittweger

    Astrium Space Transportation

    Germany

    4

    Numerical Analysis of Impact Deformation and Failure in Nanocomposite plates

    Prof. Leo Daniel

    Massachusetts Institute of Technology (MIT)

    United States

    5

    Computational intelligent satellite attitude control design

    presentation

    Dr. Ernesto Araujo

    Instituto Nacional de Pesquisas Espaciais (INPE)

    Brazil

    6

    Effect of Space Vehicle Structure Vibration on Control Moment Gyroscope Dynamics

    presentation

    Dr. Tatiana Dobrinskaya

    United Space Alliance

    United States

    7

    LSS Vibratinal/Rotational Control Taking Into Account the Thermal Effects on the PZT Sensor Output Signals

    presentation

    Dr. Ijar M. Da Fonseca

    Instituto Nacional de Pesquisas Espaciais (INPE) and UNINOVE University

    Brazil

    8

    TRUE AND EFFICIENT SOLUTION OF BEM-FEM ACOUSTIC-STRUCTURAL COUPLING FOR UNIFIED SPACECRAFT FLUID-STRUCTURE COUPLING USING CHIEF REGULARIZATION AND FAST MULTIPOLE EXPANSION

    presentation

    Prof. Harijono Djojodihardjo

    Universitas Al Azhar Indonesia

    Indonesia

    9

    study of estimation method of microvibration with simulated satellite structure

    presentation

    Mr. Osamu Takahara

    Mitsubishi Electric Corporation

    Japan

    10

    Characterization and verification of micro-vibration environment in GOCE satellite

    presentation

    Mr. ROBERTO ULLIO

    Thales Alenia Space Italia

    Italy