IAF Digital Library

3

session 3

Title: Space Structures - Dynamics and Microdynamics
Description: The topics to be addressed include 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: 2011-10-04
Time: 15:00
Room: TS-17

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	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		SANTINI MEMORIAL LECTURE: Space Challenges and Opportunities for Human Benefit	40	confirmed	Dr. Michael Yarymovych		United States
2		Control-oriented Modelization of a Satellite with Large Flexible Appendages and Use of Worst-Case Analysis to Verify Robustness to Model Uncertainties of Attitude Control	20	confirmed	Prof. Paolo Gasbarri	Università di Roma "La Sapienza"	Italy
3		CSI Interaction due to a Stepper motor Actuation on a LEO LSS Solar Panel	20	confirmed	Dr. Ijar M. Da Fonseca	Instituto Nacional de Pesquisas Espaciais (INPE) and UNINOVE University	Brazil
4		Evaluation of First Stage Deployment of Membrane of IKAROS Based on Flight Results and Simulation	20	confirmed	Dr. Yoji Shirasawa	Japan Aerospace Exploration Agency (JAXA)	Japan
5		parameters design of vibration isolation platform for control moment gyroscopes	20	confirmed	Dr. Yao Zhang	Beijing Institute of technology(BIT)	China
6		Shape control of large reflecting structures in space	20	confirmed	Prof. Anatoliy Alpatov	Institute of Technical Mechanics of the National Academy of Science and State Space Agency of Ukraine	Ukraine
7		STUDY ON DYNAMIC MODELING AND NEURAL NETWORK CONTROL FOR FREE-FLOATING SPACE FLEXIBLE-JOINT ROBOT TO TRACK DESIRED TRAJECTORY IN JOINT SPACE	20	no-show	Dr. Jie Liang		China
8		The new Appoach for Damping Modelling in the Coupled Dynamic Load Analysis for the Ariane 5 Acoustic Booster Mode Load Cases	20	confirmed	Dr. Andreas Rittweger	Astrium Space Transportation	Germany
9		FAST MULTIPOLE BOUNDARY ELEMENT SCHEME DEVELOPMENT AND INTEGRATION TO BE-FE ACOUSTIC-STRUCTURAL COUPLING	20	confirmed	Prof. Harijono Djojodihardjo	Universitas Al Azhar Indonesia	Indonesia
10		Modeling Microvibrations Transmission in Spacecraft Structures	20	confirmed	Mr. Marcello Remedia	University of Southampton	United Kingdom