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

Co-Chair: Dr. Junjiro Onoda, ISAS/JAXA, Japan;
Co-Chair: Prof. Pavel M. Trivailo, RMIT University, Australia, Australia;
Rapporteur: Prof. Paolo Gaudenzi, Sapienza University of Rome, Italy;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	Decentralized Vibration Control of a Multi-Link Flexible Robotic Manipulator using Smart Piezoelectric Transducers	15'	confirmed	Dr. Dunant Halim	University of Nottingham China	China
2	Inflatable shape changing colonies assembling versatile smart space structures	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	15'	confirmed	Dr. Xi Lu	Shanghai Institute of Satellite Engineering	China
4	Shape-Changing Solar Sails for Novel Mission Applications	15'	confirmed	Mr. Andreas Borggräfe	University of Strathclyde	United Kingdom
5	Surface Control of Active Hybrid Space Mirrors	15'	withdrawn	Dr.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	15'	confirmed	Mr. Zhang Yongliang		China
7	Wireless Strain Sensing System for Structural Health Monitoring under Various Gravity Level	15'	withdrawn	Ms. Yayu Monica Hew		United States
8	ROV-E Activities at Southampton University	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	15'	confirmed	Mr. haisheng wu	Beijing Spacecrafts, P. R. China	China
10	multi-functional piezoelectric space vehicle structural system	15'	confirmed	Mr. Judin Narlely	SRM University, kattankulathur,chennai	India
11	Adaptive Deformable Skin Resistant to High Temperature Technology Research	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	15'		Mr. Liangliang Lv	Aerospace System Engineering Shanghai, China	China

session 5

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