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: 2017-09-27
Time: 14:45
Room: Panorama Room 2

IPC members

Co-Chair: Prof. Pavel M. Trivailo, RMIT University, Australia, Australia;
Co-Chair: Dr. Hiroshi Furuya, Japan;
Rapporteur: Prof. Paolo Gaudenzi, Sapienza University of Rome, Italy;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	Demonstration of Sparse Aperture Configuration for Imaging Satellites	12	confirmed	Dr. Brij Agrawal	Naval Postgraduate School	United States
2	Design of a smart tailored stiffness nonlinear spring	12	confirmed	Mr. Mohammed K. Abbas	Northwestern Polytechnical University	China
3	Novel 2-collinear-DoF strut prototype for spacecraft micro-vibration mitigation	12	confirmed	Mr. Alessandro Stabile	University of Surrey	United Kingdom
4	implementation and application of digital-controlled piezoelectric vibration absorbers to truss structures	12	confirmed	Mr. Satoshi Yamada	Osaka Prefecture University	Japan
5	Augmented Adaptive Motion Control and Vibration Optimal Control for Free-floating Flexible Space Manipulators with An Elastic Base	12	withdrawn	Dr. xiaoyan yu	Fuzhou University	China
6	Modeling and design of a nonlinear aeroelastic energy harvester	12	confirmed	Dr. Marco Eugeni	Università di Roma "La Sapienza"	Italy
7	A Novel Shape Memory Alloy Actuator for Solar Sailing Attitude Control	12	confirmed	Dr. Xiaofeng Wu	The University of Sydney	Australia
8	evaluation of optical properties of advanced reflectivity control device for solar sail by numerical simulation	12	confirmed	Mr. Hirokazu Ishida	The University of TOKYO, Graduate school	Japan
9	Attitude control of a rigid flexible satellite by using reaction wheel and piezoelectric material for passive control of the elastic vibration	12	confirmed	Dr. Ijar M. Da Fonseca	ITA-DCTA	Brazil
10	digital construction system for scalable space infrastructure	12	withdrawn	Mr. Benjamin Jenett	Massachusetts Institute of Technology (MIT)	United States
11	New thermal protection systems for space launchers: icephobic coating for cryogenic rocket engine	12	confirmed	Dr. Luca Mazzola	CIRA Italian Aerospace Research Centre	Italy
12	Characterizing the Pyroelectric Coefficient for Macro-Fiber Composites	12	withdrawn	Ms. Krystal Acosta	University of Michigan	United States
13	Use of smart material for efficient and safer sub orbital space flights	12	no-show	Mr. AMANJOT SINGH		India
14	fiber bragg grating sensing system for long-term health monitoring of aerospace structures	12	withdrawn	Ms. Shengnan Geng		China

session 5

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