session 2

Title

Space Structures II - Development and Verification (Deployable and Dimensionally Stable Structures)

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
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

4th PAOLO SANTINI MEMORIAL LECTURE: DYNAMICS MODELING AND CONTROL OF FLEXIBLE SPACE MANIPULATORS

accepted

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

accepted

12'

confirmed

Dr. Ijar M. Da Fonseca

ITA-DCTA

Brazil

3

3d minimum reaction control for space manipulators

accepted

12'

confirmed

Mr. Daniele Pagnozzi

University of Strathclyde

United Kingdom

4

Importance of structural damping in the dynamic analysis of compliant deployable structures

accepted

12'

confirmed

Ms. Florence Dewalque

University of Liège

Belgium

5

modified multi-particle model of space membrane structures considering mechanical characteristic of creases

accepted

12'

confirmed

Mr. Ryota Inoue

Hokkaido University

Japan

6

A Robotically-Assembled 100-meter Space Telescope

accepted

12'

confirmed

Ms. Kristina Hogstrom

California Institute of Technology

United States

7

buckling and wrinkling of inflatable support structure of deployable antenna

accepted

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

accepted

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

accepted

12'

confirmed

Mr. YUTA KUSANO

Tokai University

Japan

10

Design of tape spring hinges for solar array considering deployment performances

accepted

12'

confirmed

Mr. Kyung-Won Kim

Korea Aerospace Research Institute (KARI)

Korea, Republic of

11

Mesh deployable antenna mechanics testing method

accepted

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

accepted

12'

confirmed

Dr. Liu Dali

Aerospace System Engineering Shanghai

China

design and buckling analysis for support ribs of inflatable antenna reflector

merged with 21842

confirmed

Dr. Zhenmeng Xia

Harbin Institute of Technology

China