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: 2009-10-13
Time: 15:00
Room: Technical Session #5

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	combined load analysis of satellite and rocket	16'	Mr. Seung Yong Min	Seoul National University	Korea, Republic of
2	INTERNAL LOADING DISTRIBUTION IN STATICALLY LOADED BALL BEARINGS SUBJECTED TO A COMBINED RADIAL, THRUST, AND MOMENT LOAD	16'	Dr. Mário Ricci	INPE	Brazil
3	Optimal Manoeuvring of a Flexible Space Manipulator with Respect to a Class of Objectives	16'	Dr. Chiara Toglia	University of Rome “La Sapienza”	Italy
4	Real-time Optimal Collision-Free Control for Robotic Arm Manipulators in the Presence of Wandering Obstacles	16'	Prof. Pavel M. Trivailo	RMIT University, Australia	Australia
5	APPLICATION OF FAST MULTIPOLE BOUNDARY ELEMENT METHOD FOR UNIFIED FMBEM-FEM ACOUSTIC-STRUCTURAL COUPLING	16'	Prof. Harijono Djojodihardjo	Universitas Al Azhar Indonesia	Indonesia
6	experimental investigation on thermally induced vibration of flexible boom in space environment using vacuum chamber	16'	Mr. hyun bum park		Korea, Republic of
8	development of scheduling algorithm and gui for the autonomous satellite mission operation	16'	Mr. SeungWoo Baek	Pusan National University	Korea, Republic of
9	Adaptive Tuned Mass Damper to Suppress Vibration of Tension-Stabilized Structures	16'	Dr. Yohsuke Nambu	Osaka Prefecture University	Japan
10	Topological and Deployment Analysis of Tetrahedron Unit Deployable Antenna	16'	Prof. Fu-Ling Guan	Zhejiang University	China
11	Optimum design of space frame and its application in satellite structure	16'	Dr. Chen Shenyan	Beihang University	China

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