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: 2014-09-30
Time: 09:45
Room: 713A

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	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	4th PAOLO SANTINI MEMORIAL LECTURE: DYNAMICS MODELING AND CONTROL OF FLEXIBLE SPACE MANIPULATORS	30'	confirmed	Prof. Arun Misra	McGill University	Canada
2	The Impact of the Non-Inertial Base Motion in the Operations of Robotic Manipulators in Orbit	12'	confirmed	Dr. Ijar M. Da Fonseca	ITA-DCTA	Brazil
3	3d minimum reaction control for space manipulators	12'	confirmed	Mr. Daniele Pagnozzi	University of Strathclyde	United Kingdom
4	Importance of structural damping in the dynamic analysis of compliant deployable structures	12'	confirmed	Ms. Florence Dewalque	University of Liège	Belgium
5	modified multi-particle model of space membrane structures considering mechanical characteristic of creases	12'	confirmed	Mr. Ryota Inoue	Hokkaido University	Japan
6	A Robotically-Assembled 100-meter Space Telescope	12'	confirmed	Ms. Kristina Hogstrom	California Institute of Technology	United States
7	buckling and wrinkling of inflatable support structure of deployable antenna	12'	confirmed	Prof.Dr. Changguo Wang	Harbin Institute of Technology	China
8	Development of a Gravity Compensation System for Prototype Tests of Deployable Space Structures by using Multi Mobile Robots	12'	confirmed	Mr. Hiroki Shigematsu	Osaka Institute of Technology	Japan
9	experimental and numerical study of structural stabilities of flare-type membrane aeroshell with inflatable ring	12'	confirmed	Mr. YUTA KUSANO	Tokai University	Japan
10	Design of tape spring hinges for solar array considering deployment performances	12'	confirmed	Mr. Kyung-Won Kim	Korea Aerospace Research Institute (KARI)	Korea, Republic of
11	Mesh deployable antenna mechanics testing method	12'	no-show	Dr. Li JIANG	China Academy of Launch Vehicle Technology (CALT)	China
12	A Bionic Structure for Flexible Solar Array via Topology Optimization	12'	confirmed	Dr. Liu Dali	Aerospace System Engineering Shanghai	China
–	design and buckling analysis for support ribs of inflatable antenna reflector		confirmed	Dr. Zhenmeng Xia	Harbin Institute of Technology	China

session 2

Order

Time

Paper title

Mode

Presentation status

Speaker

Affiliation

Country