session 3

Title: Space Structures - Dynamics and Microdynamics
type: oral
Description: Topics included in this session are: Dynamics analysis and testing, modal identification, landing and impact dynamics, pyroshock, test facilities, vibration suppression techniques, damping, micro-dynamics, in-orbit dynamic environment, wave structural propagation, excitation sources and in-orbit dynamic testing.
Date: 2008-09-30
Time: 15:00
Room: Dochart 1

IPC members

Chairman: Dr. Peter M. Bainum, Howard University, United States;
Chairman: Prof. Ijar Da Fonseca, ITA-DCTA, Brazil;
Rapporteur: Prof. Harijono Djojodihardjo, Bandung Institut of Tecnology, Indonesia;

papers
Order	Paper title	Mode	Speaker	Affiliation	Country
1	Flexibility effects in controlled behaviour of space manipulators	presentation	Dr. Chiara Toglia	University of Rome “La Sapienza”	Italy
2	Interactive Virtual Reality Simulator for the Optimally Controlled Space Robotic Manipulators	presentation	Prof. Pavel M. Trivailo	RMIT University, Australia	Australia
3	Coupled Dynamic Load Analsyis with Different Component Damping of the Substructures	presentation	Dr. Andreas Rittweger	Astrium Space Transportation	Germany
4	Numerical Analysis of Impact Deformation and Failure in Nanocomposite plates		Prof. Leo Daniel	Massachusetts Institute of Technology (MIT)	United States
5	Computational intelligent satellite attitude control design	presentation	Dr. Ernesto Araujo	Instituto Nacional de Pesquisas Espaciais (INPE)	Brazil
6	Effect of Space Vehicle Structure Vibration on Control Moment Gyroscope Dynamics	presentation	Dr. Tatiana Dobrinskaya	United Space Alliance	United States
7	LSS Vibratinal/Rotational Control Taking Into Account the Thermal Effects on the PZT Sensor Output Signals	presentation	Dr. Ijar M. Da Fonseca	Instituto Nacional de Pesquisas Espaciais (INPE) and UNINOVE University	Brazil
8	TRUE AND EFFICIENT SOLUTION OF BEM-FEM ACOUSTIC-STRUCTURAL COUPLING FOR UNIFIED SPACECRAFT FLUID-STRUCTURE COUPLING USING CHIEF REGULARIZATION AND FAST MULTIPOLE EXPANSION	presentation	Prof. Harijono Djojodihardjo	Universitas Al Azhar Indonesia	Indonesia
9	study of estimation method of microvibration with simulated satellite structure	presentation	Mr. Osamu Takahara	Mitsubishi Electric Corporation	Japan
10	Characterization and verification of micro-vibration environment in GOCE satellite	presentation	Mr. ROBERTO ULLIO	Thales Alenia Space Italia	Italy

session 3

Order

Time

Paper title

Mode

Presentation status

Speaker

Affiliation

Country