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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

    2016-09-27

    Time

    14:45

    Room

    Salon de Eventos 1

    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

    Vibration Analysis, Control and Genetic Algorithm Optimization of a Piezoelectric Elements Bonded Rotating Spacecraft Appendage Composite Structure

    15'

    confirmed

    Prof. Harijono Djojodihardjo

    Indonesia

    7

    Dynamic Load Synthesis for Shock Numerical Simulation in Space Structure Design

    15'

    confirmed

    Dr. Riccardo Monti

    Thales Alenia Space Italia

    Italy

    8

    Feasibility Study on Spaceborne Cooler Micro-vibration Energy Harvesting System using Piezoelectric

    15'

    confirmed

    Mr. Seong-Cheol Kwon

    Chosun University

    Korea, Republic of

    9

    On-orbit identification of inertia parameters of combined spacecraft using space manipulator

    15'

    confirmed

    Ms. LI Haiyan

    China

    10

    Prediction of the microvibration from Ground test and Its In-orbit evaluation of the geostationary meteorological satellite ‘HIMAWARI-8’

    15'

    confirmed

    Mr. Osamu Takahara

    Mitsubishi Electric Corporation

    Japan

    12

    Structural dynamic analysis of a nanosatellite launch platform

    15'

    confirmed

    Mr. Salvatore Paiano

    G.A.U.S.S. Srl

    Italy

    13

    Some methods for modelling multi-scale spacecrafts dynamics with SGS

    15'

    confirmed

    Prof. Lyudmila Kuzmina

    Kazan National Research Technical University

    Russian Federation

    14

    The Impact of Aero-Elastic Effects on the Controllability of Conventional Launch Vehicles

    15'

    confirmed

    Dr. Derek Gransden

    Delft University of Technology (TU Delft)

    The Netherlands