• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-17
  • C2
  • 3
  • session 3

    Title

    Space Structures - Dynamics and Microdynamics

    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

    3

    Active vibration control on a membrane solar panel for nanosatellites

    12

    withdrawn

    Ms. Laura Bettiol

    CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova

    Italy

    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)

    The Netherlands

    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

    10

    Touchdown Stability Estimation of an unmanned spacecraft on lunar regolith

    12

    no-show

    Mr. Sai Phanindra Darbha

    Team Indus, Axiom Research Labs Pvt. Ltd.

    India

    11

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

    12

    confirmed

    Mr. Seong-Cheol Kwon

    Chosun University

    Korea, Republic of

    12

    investigation of nonlinear energy sink for vibration absorption by means of homotopy analysis method

    12

    no-show

    Mr. Haiqin Li

    China