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  • session 3

    Title

    Space Structures - Dynamics and Microdynamics

    type

    oral

    Description

    The topics to be addressed include 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

    2017-09-26

    Time

    14:45

    Room

    Panorama Room 2

    IPC members
    • Co-Chair: Prof. Ijar Da Fonseca, ITA-DCTA, Brazil;

    • Co-Chair: Prof. Harijono Djojodihardjo, Bandung Institut of Tecnology, Indonesia;

    • Rapporteur: Dr. Luigi Scatteia, PricewaterhouseCoopers Advisory (PwC), France;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Prediction of Vibration Characteristics of Variable Diameter Shell Composite Structure via 2D Sub-scale Modeling

    12

    confirmed

    Mr. BEHZAD AHMED ZAI

    Pakistan Space and Upper Atmosphere Research Commission (SUPARCO)

    Pakistan

    2

    proposal of a method to detect buckling and unstable deformation in dynamic analysis

    12

    confirmed

    Dr. Shoko Arita

    Shizuoka University

    Japan

    4

    METHODOLOGY OF EVALUATION THE INFLUENCE OF SMALL ASYMMETRY EXTERNAL FORMS OF SPACE LANDING VEHICLE ON A DEVIATION OF THE LONGITUDINAL AXIS AT MOVEMENT UNDER RESONANT MODE

    12

    confirmed

    Dr. Vsevolod Koryanov

    Bauman Moscow State Technical University

    Russian Federation

    5

    Tuning Guideline for a Shock Test Facility for Spacecraft Equipment Qualification

    12

    confirmed

    Mr. Andreas Dueck

    RWTH Aachen University

    Germany

    6

    Vibration Analysis, Control And Optimization of a Piezoelectric Elements Bonded Flexural - Torsional Composite Beam

    12

    confirmed

    Prof. Harijono Djojodihardjo

    Indonesia

    7

    Quasi-Transient Stability Analysis of a Conventional Aeroelastic Launch Vehicle

    12

    confirmed

    Dr. Derek Gransden

    Delft University of Technology (TU Delft)

    Netherlands (Kingdom of the)

    8

    Elastic deformation modeling of the VS-40m suborbital rocket with SARA payload

    12

    confirmed

    Dr. ELCIO JERONIMO DE OLIVEIRA

    Institute of Aeronautics and Space (IAE)

    Brazil

    9

    Modal Parameter Characterization for a Small Scale Heliogyro Blade in High Vacuum Chamber

    12

    confirmed

    Mrs. Sarah Cook

    University of Colorado Boulder

    United States

    11

    A Synchronized Switching Strategy to Increase Energy Harvesting Efficiency from Micro-scale Vibration Energy

    12

    confirmed

    Mr. Seong-Cheol Kwon

    Chosun University

    Republic of Korea