IAF Digital Library

3

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: 2014-09-30
Time: 14:45
Room: 713A

IPC members

Co-Chair: Dr. Peter M. Bainum, Howard University, United States;
Co-Chair: 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		Decomposition methods in multiscale dynamics of spacecrafts with SGS	12'	confirmed	Prof. Lyudmila Kuzmina	Kazan National Research Technical University	Russian Federation
2		inspecting the characterisation of microvibration sources	12'	confirmed	Mr. Daniele Addari	Surrey Space Centre, University of Surrey	United Kingdom
3		Landing capsule soft touchdown dynamics	12'	confirmed	Mr. Vitalii Voronin	S.P. Korolev Rocket and Space Corporation Energia	Russian Federation
4		Method of calculating the descent of the spacecraft in the atmosphere using technology adaptation landing in different environmental conditions	12'	confirmed	Dr. Vsevolod Koryanov	Bauman Moscow State Technical University	Russian Federation
5		Dynamic/control interactions between flexible orbiting space-robot during grasping, docking and post-docking maneuvers	12'	confirmed	Prof. Paolo Gasbarri	Università di Roma "La Sapienza"	Italy
6		evaluation of transient response of spinning solar sail with flexible membrane by eigenfunction analysis and continuum analysis	12'	confirmed	Mr. Toshihiro Chujo	The University of TOKYO, Graduate school	Japan
7		Predicting optical instrument performance under micro-vibrations	12'	confirmed	Dr. Stefan Bedrich	OHB System AG - Munich	Germany
8		Vibration Analysis of a Cantilevered Beam with Piezo-Electric Actuator at the Tip as a Controllable Elastic Structure	12'	confirmed	Prof. Harijono Djojodihardjo	Universitas Al Azhar Indonesia	Indonesia
9		Surface Shape Measurement of Vibrating Membrane induced by Impact Loading	12'	confirmed	Dr. Takashi Iwasa	Tottori University	Japan
10		deployment dynamics of membrane-boom wrapped structures	12'	confirmed	Prof. Hiroshi Furuya	Tokyo Institute of Technology	Japan
11		Bending mode propagation in shock analysis using axis symmetrical shell elements time explicit solution and spectral elements	12'	withdrawn	Mr. Bernhard Kotzias	EADS Space	Germany
12		Distributed passive and active vibration control for spacecraft with large flexible appendage	12'	confirmed	Dr. Yao Zhang	Beijing Institute of technology(BIT)	China
13		investigations on representation of the interface boundary conditions of an earth observation satellite	12'	confirmed	Mr. Baris Eroglu	TAI - Turkish Aerospace Industries, Inc.	Türkiye
–		Hybrid robust control of a free-flying flexible space manipulator		confirmed	Dr. xiaoyan yu	Fuzhou University	China