session 3

Title: Space Structures - Dynamics and Microdynamics
type: oral
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: 2010-09-28
Time: 15:15
Room: Meeting Room 42

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	Presentation status	Speaker	Affiliation	Country
1	Experimental verification of damage detection based on proper orthogonal decomposition on a plate structure	20		Dr. Mirco Zaccariotto	CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova	Italy
2	MICRO-VIBRATION MEASUREMENTS ON THERMALLY LOADED MULTI-LAYER INSULATION SAMPLES	20	confirmed	Dr. Anton Grillenbeck	IABG Industrieanlagen - Betriebsgesellschaft mbH	Germany
3	A Technique of Reaction Wheel Control for Precise Torque Transmission in Suppressing Its Own Disturbance	20	withdrawn	Mr. Takanori Toraya	Tokyo Metropolitan University	Japan
4	FURTHER DEVELOPMENT IN THE APPLICATION OF FAST MULTIPOLE BOUNDARY ELEMENT METHOD FOR UNIFIED BEM-FEM ACOUSTIC-STRUCTURAL COUPLING	20	confirmed	Prof. Harijono Djojodihardjo	Universitas Al Azhar Indonesia	Indonesia
5	flexural wave scattering by multiple elliptic holes in an infinite thin plate	20	confirmed	Prof. Hongliang Li	Harbin Engineering University	China
6	VIBRATION CONTROL OF A FLEXIBLE SPACE MANIPULATOR DURING ON ORBIT OPERATIONS	20	confirmed	Prof. Paolo Gasbarri	Università di Roma "La Sapienza"	Italy
7	Placement Optimization of Piezoelectric Sensors in a Clamped-free Plate Like Solar Panel on a Large Space Structure	20	confirmed	Dr. Ijar M. Da Fonseca	Instituto Nacional de Pesquisas Espaciais (INPE) and UNINOVE University	Brazil
8	geometrically exact 3d beam element for arbitrary large rigid-elastic deformation analysis of aerospace structures	10	withdrawn	Mr. Genyong Wu	Northwestern Polytechnical University	China
9	Research on Methodology of Aeroservoelastic Stability Analysis for Reusable Launch Vehicle	10	confirmed	Mr. Junpeng Hui	China Academy of Launch Vehicle Technology (CALT)	China
10	study on fluid-structure interaction in liquid rocket feed system	10	confirmed	Mr. Xin Wei	Beijing University of Aeronautics and Astronautics (BUAA)	China
11	Prediction for Shock Behavior of Satellite Structure Panel Based on Numerical Analysis	10	confirmed	Ms. Hanui Jeong	Chungnam National University	Korea, Republic of

session 3

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