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

2012-10-03

Time

15:15

Room

TS07 (Sala Regulus, Hall 3)

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Bio-inspired programmable matter for space applications

accepted

15'

confirmed

Mr. Thomas Sinn

University of Strathclyde/Advanced Space Concepts Laboratory

United Kingdom

2

NOVEL KINEMATIC CONTROL TECHNIQUE FOR ELECTROACTIVE POLYMER ROLLING ROVERS

accepted

15'

withdrawn

Dr. Silvio Cocuzza

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

Italy

3

Shape Control of a Membrane Structure with Shape Memory Alloys

accepted

15'

confirmed

Mr. Ryan Orszulik

York University

Canada

4

Applications of Tuned Mass Dampers to Improve Performance of Large Space Mirrors

accepted

15'

confirmed

Dr. Brij Agrawal

Naval Postgraduate School

United States

5

Vibration control for membrane by smart dynamic vibration absorber

accepted

15'

confirmed

Mr. Shota Yamamoto

Osaka Prefecture University

Japan

6

Fuzzy-based Adaptive Multi-modal Vibration Control with Imperfect Structural Data

accepted

15'

confirmed

Prof. Kanjuro Makihara

Tohoku University

Japan

7

Wireless structural health monitoring of space structures with energy harvesting capabilities

accepted

15'

withdrawn

Mr. Luca Lampani

University of Rome “La Sapienza”

Italy

8

Wireless Strain Sensing System for Spacecraft Health Monitoring

accepted

15'

confirmed

Ms. Yayu Monica Hew

United States

9

Design of a Fiber-Optic Interrogator Module for the Hybrid Sensor Bus System for Temperature Monitoring in Telecommunication Satellites

accepted

15'

no-show

Mr. Philipp Putzer

Technical University of Munich

Germany

10

FIBER-OPTIC STRAIN SENOR-BASED STRUCTURAL HEALTH MONITORING OF AN UNINHABITATED AIR VEHICLE

accepted

15'

no-show

Mrs. Jessica Alvarenga

California State University, NASA URC SPACE Center

United States

11

A distributed strain surveillance system for cryogenic tank

accepted

15'

no-show

Dr. peng weibin

Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

China