IAF Digital Library

6

session 6

Title: Attitude Dynamics - Part 2
type: oral
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: 2011-10-06
Time: 10:00
Room: TS-04

IPC members

Chairman: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;
Chairman: Prof. Gerard Gomez, University of Barcelona, Spain;
Rapporteur: Mrs. Amalia Ercoli Finzi, Politecnico di Milano, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Modular Simulation and Visualisation Application for Satellite Attitude Control	15	confirmed	Mr. Lourens Visagie	Surrey Space Centre, University of Surrey	United Kingdom
2		Testing strategies for verifying the slew rate tolerance in star trackers	15	confirmed
3		Space Station Attitude Control/Momentum Management Controller Design Based on theta-D Technique	15	confirmed	Mrs. Mengping Zhu	Beihang University	China
4		Novel strategies to increase robustness in the reaction control of space manipulators: theory and simulated microgravity tests	15	confirmed	Dr. Stefano Rossi	Swiss Space Center	Switzerland
5		Singular perturbation and fuzzy variable structure sliding mode control of space robot system with flexible joint in inertial space	15	no-show	Dr. Limin Xie	Fuzhou University	China
6		Command Shaping for Nonlinearity Compensation of Reaction Wheels in Spacecrafts	15	withdrawn	Dr. Seon-Ho Lee	Korea Aerospace Research Institute (KARI)	Korea, Republic of
7		A novel APS star tracker for pico- and nano-satellites	15	confirmed	Mr. Harald Wojtkowiak	University Wuerzburg	Germany
8		Computationally light attitude controls for resource limited nano-spacecraft	15	confirmed	Mr. Craig Maclean	Advanced Space Concept Laboratory, University of Strathclyde	United Kingdom
9		Estimation of Attitude and Modal Coordinates for Spacecraft Attitude Control with Non-collocated Sensors and Actuators	15	withdrawn	Mr. Heng Shi	Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)	China
10		HARDWARE-IN-THE-LOOP TESTING OF A REACTION WHEEL VIA SLIDING MODE SPEED CONTROLLER	15	no-show	Mr. Mohammad Hossein Beheshti	K. N. Toosi University of Technology	Iran
11		Solar Sail Attitude Control using Centre of Mass/Centre of Pressure offset techniques	15	withdrawn	Mr. Theodoros Theodorou	Surrey Space Centre, University of Surrey	United Kingdom