session 8

Title: Attitude Dynamics (1)
Description: This theme discusses advances in spacecraft attitude dynamics and control, as well as attitude sensors and actuators. The theme also covers dynamics and control of multiple interconnected rigid and flexible bodies including tethered systems and space robots.
Date: 2012-10-05
Time: 09:00
Room: TS01 (Sala Aldebaran, Hall 1)

IPC members

Chairman: Prof. Gianmarco Radice, Singapore, Republic of;
Chairman: Prof.Dr. Kazuya Yoshida, Tohoku University, Japan;
Rapporteur: Dr. Simei Ji, Beijing Institute of Technology, China;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		COUPLED ORBIT AND ATTITUDE DYNAMICS FOR A SPACECRAFT COMPRISED OF MULTIPLE BODIES IN EARTH-MOON HALO ORBITS	accepted	15'	confirmed	Ms. Amanda Knutson	Purdue University	United States
2		AOCS science mode design for ESA’s EUCLID mission	accepted	15'	withdrawn	Mr. Alberto Anselmi	Thales Alenia Space Italia	Italy
3		Zero-propellant attitude maneuver path planning of space station based on simple gimbal control moment gyroscopes	accepted	15'	confirmed	Dr. Hai-bing Huang	National University of Defense Technology	China
4		Robustness Analyses of Attitude Slew Manoeuvres for Spinning Penetrator Spacecraft	accepted	15'	confirmed	Mr. Robin Raus	EADS Astrium	United Kingdom
5		REX-J (Robot Experiment on ISS/JEM) to demonstrate astronaut support robot - Result of the in-orbit check out of the REX-J mission	accepted	15'	confirmed	Prof.Dr. Mitsushige Oda	JAXA	Japan
6		Development of sun-pointing magnetic attitude control system for cxbn cubesat	accepted	15'	confirmed	Mr. Paride Testani	Scuola Ingegneria Aerospaziale	Italy
7		Dynamic Modelling and Control of Flexible Robotic Space Manipulators with Telescoping Booms	accepted	15'	confirmed	Mr. Alex Walsh	McGill University	Canada
8		First in-orbit results of the Pleiades CMG-based attitude control system	accepted	15'	confirmed	Dr. Charles Koeck	EADS Astrium	France
9		Space manipulator control for the DYMAFLEX flight experiment	accepted	15'	confirmed	Mr. Nicholas D'Amore	University of Maryland, College Park	United States
10		Investigation of On-Orbit Electodynamic Tether Deployment by Ground Experiment and Numerical Simulation using a Detailed Friction Model	accepted	15'	confirmed	Mr. Mitsuhisa Baba	Waseda University	Japan
11		Experimental orbital rendezvous operations via visual based techniques	accepted	15'	confirmed	Dr. Marco Sabatini	Sapienza University of Rome	Italy
12		Path planning of experimental module transfer for minimizing attitude disturbance of space station	accepted	15'	withdrawn	Mr. Yi Wang	National University of Defense Technology	China
13		A Sensitivity Analysis Approach in the Design of the Attitude Control System of Small Satellites	accepted	15'	confirmed	Prof. Teodor-Viorel Chelaru	University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space	Romania