session 2

Title: Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)
type: oral
Description: The topics to be addressed include evaluation of analysis versus test results for deployable and dimensionally stable structures, e.g. reflectors, telescopes, antennas; examination of both on-ground and in-orbit testing, thermal distortion and shape control, structural design, development and verification; lessons learned.
Date: 2016-09-27
Time: 09:45
Room: Salon de Eventos 1

IPC members

Co-Chair: Prof. Paolo Gasbarri, University of Rome “La Sapienza”, Italy;
Co-Chair: Mr. Jean-Alain Massoni, Thales Alenia Space France, France;
Rapporteur: Prof. Pierre Rochus, CSL (Centre Spatial de Liège), Belgium;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	PAOLO SANTINI MEMORIAL LECTURE: Half a century of Space Adventure at Centre Spatial of Liège	30'	confirmed	Prof. Pierre Rochus	CSL (Centre Spatial de Liège)	Belgium
2	10:15	DEVELOPMENT OF DIMENSIONALLY STABLE STRUCTURE OF DRAWTUBE OF OPTICAL DEVICE OF COMPOSITE MATERIAL	15'	confirmed	Ms. Antonina Kulik	Yuzhnoye State Design Office	Ukraine
3	10:30	Verification Testing of the Gossamer-1 Deployment Demonstrator	15'	no-show	Mr. Jan Thimo Grundmann	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
4	10:45	impedance control of a multi-arm space robot for capturing a non-cooperative target	15'	no-show	Mr. Angelo Stolfi	Università di Roma "La Sapienza"	Italy
5	11:00	A High-accuracy Micro-deformation Measurement Method for High-resolution Space Camera Complex Structured	15'	no-show	Dr. Li JIANG	China Academy of Launch Vehicle Technology (CALT)	China
6	11:15	The research of the vibration reliability of the ceramic packaging BGA and CGA devices	15'	withdrawn	Dr. Wei Zhang	China Academy of Launch Vehicle Technology(CALT)	China
7	11:30	Attitude and vibration control of a satellite containing flexible solar arrays by using reaction wheels, thrusters, and piezoelectric transducers as sensors and actuators.	15'	confirmed	Dr. Ijar M. Da Fonseca	ITA-DCTA	Brazil
8	11:45	Ground Experiments of Boom-membrane Integrated Deployable Structures for Micro Satellites	15'	withdrawn	Prof. Hiroshi Furuya	Tokyo Institute of Technology	Japan
9	12:00	A Modular and Efficient System for Antenna Deployment in Swayam: A Platform for Reliable Bi- Directional Communication	15'	withdrawn	Ms. Tanvi Katke	College of Engineering, Pune	India
10	12:15	a study on the asymmetric spinning deployment of membrane structure with variation thickness	15'	confirmed	Mr. Hiroyuki Kinoshita	Tokai University	Japan
11	12:30	Design and ground test of the isolator for satellite attitude control actuator	15'	confirmed	Mr. Jia Tian	China Academy of Space Technology (Xi’an), CAST	China
12	12:45	FBG optical sensors for environmental tests of microsatellites	15'	confirmed	Dr. Giampiero Sindoni	Sapienza University of Rome	Italy
13	13:00	Topology optimization and FDM prototyping of bionic inspired strengthening-ribs in membranes of spacecraft	15'	confirmed	Prof. Qingxi Hu	Shanghai University	China

session 2

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