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

2013-09-25

Time

14:45

Room

306B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Decentralized Vibration Control of a Multi-Link Flexible Robotic Manipulator using Smart Piezoelectric Transducers

accepted

15'

confirmed

Dr. Dunant Halim

University of Nottingham China

China

2

Inflatable shape changing colonies assembling versatile smart space structures

accepted

15'

confirmed

Mr. Thomas Sinn

University of Strathclyde/Advanced Space Concepts Laboratory

United Kingdom

3

Research on Guided Wave based Structural Health Monitoring techniques for Deep Space Explorer

accepted

15'

confirmed

Dr. Xi Lu

Shanghai Institute of Satellite Engineering

China

4

Shape-Changing Solar Sails for Novel Mission Applications

accepted

15'

confirmed

Mr. Andreas Borggräfe

University of Strathclyde

United Kingdom

5

Surface Control of Active Hybrid Space Mirrors

accepted

15'

withdrawn

Dr. Brij Agrawal

Naval Postgraduate School

United States

6

The performance research of the metal rubber vibration isolator for Whole-Spacecraft Vibration Suppression

accepted

15'

confirmed

Mr. Zhang Yongliang

China

7

Wireless Strain Sensing System for Structural Health Monitoring under Various Gravity Level

accepted

15'

withdrawn

Ms. Yayu Monica Hew

United States

8

ROV-E Activities at Southampton University

accepted

15'

confirmed

Dr. James Foster

University of Southampton

United Kingdom

9

research on the application of fiber bragg gratings sensors for structural health management of composites in spacecraft

accepted

15'

confirmed

Mr. haisheng wu

Beijing Spacecrafts, P. R. China

China

10

multi-functional piezoelectric space vehicle structural system

accepted

15'

confirmed

Mr. Judin Narlely

SRM University, kattankulathur,chennai

India

11

Adaptive Deformable Skin Resistant to High Temperature Technology Research

accepted

15'

confirmed

Mr. Shiyong Huang

China Academy of Launch Vehicle Technology (CALT)

China

12

actuators location optimization and active vibration control of large flexible space structures

accepted

15'

Mr. Liangliang Lv

Aerospace System Engineering Shanghai, China

China