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  • session 5

    Title

    Smart Materials and Adaptive Structures

    Description

    The focus of the session will be on application of smart materials to spacecraft and launch vehicle systems, novel sensor and actuator concepts and new concepts for multi- functional and intelligent structural systems. Also included in the session will be new control methods for vibration suppression and shape control using adaptive structures as well as comparisons of predicted performance with data from ground and in-orbit testing.

    Date

    2016-09-28

    Time

    14:45

    Room

    Salon de Eventos 1

    IPC members
    • Co-Chair: Prof. Pavel M. Trivailo, RMIT University, Australia, Australia;

    • Co-Chair: Prof. Hiroshi Furuya, Tokyo Institute of Technology, Japan;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Impact of Large Field Angles on the Requirements for Deformable Mirrors in Imaging Satellites

    15'

    confirmed

    Dr. Brij Agrawal

    Naval Postgraduate School

    United States

    2

    an optimization of ssdi system for a beam structure

    15'

    confirmed

    Mr. Shigeru Shimose

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    A SMA wire actuated hold-down and release device using two ball lock mechanisms

    15'

    withdrawn

    Dr. Xiaoyong Zhang

    Beihang University (BUAA)

    China

    4

    Development of a Composite Based Wiring Technique for Small Satellite Applications

    15'

    withdrawn

    Mr. Ravi Vishwanath Mangipudi

    Indian Institute of Science

    India

    5

    New Application of Shape Memory Alloy Spring Actuator to Calibration Mechanism with Dual-function of Launch Locking and Fail-safe

    15'

    confirmed

    Mr. Myeong-Jae Lee

    Chosun University

    Korea, Republic of

    6

    Multiple Failure Modes-coupled Piezoelectric Vibration Inhibition System Layout Optimization

    15'

    no-show

    Dr. lin ye

    China

    7

    Location Of A Maximum Deflection Point With Fiber Bragg Gratings In Polarization-Maintaining Optical Fiber

    15'

    withdrawn

    Mr. Joel Quintana

    University of Texas at El Paso

    United States

    8

    shape memory alloys for space debris capture applications

    15'

    confirmed

    Mr. Louis Wei-yu Feng

    University of Cape Town

    South Africa

    9

    Robust Motion Control and Vibration Optimal Control for a Free-flying Flexible Space Manipulator with Elastic Base

    15'

    confirmed

    Dr. xiaoyan yu

    Fuzhou University

    China

    10

    dynamic impact characteristics of defective functionally graded honeycombs

    15'

    withdrawn

    Prof. Tao Fan

    Harbin Engineering University

    China

    11

    Propagation characteristics of acoustic emission wave in a cylindrical composite cabin with variable diameters

    15'

    no-show

    Dr. Denghong Xiao

    Beijing Electro-Mechanical Engineering Institute, China Aerospace Science & Industry Corporation (CASIC)

    China

    12

    Dynamics and control of a flexible clamped-free beam on a rotating hub by using the state-dependent Riccati equation (SDRE) strategy

    15'

    confirmed

    Mr. Vinicius Piro Barragam

    ITA-DCTA

    Brazil