session 9

Title: Attitude Dynamics (2)
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: 14:00
Room: TS01 (Sala Aldebaran, Hall 1)

IPC members

Chairman: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;
Chairman: Bang Hyochoong, Korea Advanced Institute of Science and Technology (KAIST), Korea, Republic of;
Rapporteur: Mrs. Amalia Ercoli Finzi, Politecnico di Milano, Italy;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Neural-Network-Based Wide-FOV CMOS Sun Sensor	accepted	15'	confirmed	Prof. Michele Grassi	University of Naples "Federico II"	Italy
2		Practical approach for quick attitude maneuver of spacecraft with actuator saturation	accepted	15'	confirmed	Mr. Hyosang Yoon	Satrec Initiative	Korea, Republic of
3		SDS-4 Attitude Control System: First Flight Results of Attitude Control Response	accepted	15'	confirmed	Mr. Yuta Nakajima	Japan Aerospace Exploration Agency (JAXA)	Japan
4		Dynamics of a tether connected to an Irregular Shaped Celestial Body	accepted	15'	confirmed	Mr. Mohammad J. Mashayekhi	McGill University	Canada
5		RACS QFR Algorithm for VEGA FPSA Program	accepted	15'	confirmed	Mr. Giovanni Cuciniello	CIRA Italian Aerospace Research Centre	Italy
6		Dual Attitude and Parameter Estimation of Passively Magnetically Stabilized Spacecraft	accepted	15'	confirmed	Mr. Roland Burton	Stanford University	United States
7		Attitude motion planning for a spin stabilised disk sail	accepted	15'	confirmed	Mr. Craig Maclean	Advanced Space Concept Laboratory, University of Strathclyde	United Kingdom
8		Controllability of Propellant-free Attitude Control System for Spinning Solar Sail Using Thin-Film Reflectivity Control Devices Considering Arbitrary Sail Deformation	accepted	15'	confirmed	Prof. Ryu Funase	University of Tokyo	Japan
9		Coupled Orbital and Attitude Control of Spacecraft in Formation	accepted	15'	withdrawn	Mr. Mattia Zamaro	Politecnico di Milano	United Kingdom
10		Coupled Orbit and Attitude Dynamics of a Reconfigurable Spacecraft with Solar Radiation Pressure	accepted	15'	confirmed	Mr. Andreas Borggräfe	University of Strathclyde	United Kingdom
11		Attitude Determination Of About One Degree accuracy Using only Magnetometer Data In Megha-Tropiques	accepted	15'	confirmed	Mr. Nitin Ghatpande	Indian Space Research Organization (ISRO)	India
12		Development, complex investigation, laboratory and flight testing of the magneto-gyroscopic ACS for the microsatellite	accepted	15'	confirmed	Prof. Michael Yu Ovchinnikov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
13		Optimal Attitude Maneuver Path Planning for Spacecraft under Complex Geometry Constraints	accepted	15'	confirmed	Dr. Qian Zhao	National University of Defense Technology	China