session 3

Title: Attitude Dynamics (1)
Description: This theme discusses advances in spacecraft attitude dynamics and control, as well as design, testing and performance of novel attitude sensors and actuators. This theme also covers dynamics and control of multiple interconnected regidi and flexible bodies, including tethered systems, an in-orbit assembly.
Date: 2014-09-30
Time: 14:45
Room: 801A

IPC members

Co-Chair: Prof. Amalia Ercoli Finzi, Politecnico di Milano, Italy;
Co-Chair: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;
Rapporteur: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		new one-axis magnetic attitude control in absence of magnetometer readings	accepted	15'	confirmed	Dr. Stepan Tkachev	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
2		autonomous spacecraft attitude constraints avoidance	accepted	15'	confirmed	Mr. Ofer Salama	Rafael Advanced Defense Systems Ltd.	Israel
3		An Angular Momentum Ring Storage Device for Small Satellites Based on a Liquid Metal Actuator	accepted	15'	confirmed	Mr. Daniel Noack	Technische Universität Berlin	Germany
4		Attitude Control of Large Gossamer Spacecraft using Surface Reflectivity Modulation	accepted	15'	confirmed	Mr. Andreas Borggräfe	University of Strathclyde	United Kingdom
5		THRUSTER FAULT DETECTION ISOLATION AND RECONFIGURATION FOR INDIAN MARS ORBITER	accepted	15'	confirmed	Ms. shubha kapoor	Indian Space Research Organization (ISRO)	India
6		Practical consideration of spacecraft attitude and rate determination using numerical Gyros	accepted	15'	confirmed	Dr. Hao-Chi Chang	National Space Organization	Taiwan, China
7		BepiColombo: Dynamics analysis following module separation	accepted	15'	confirmed	Mr. Frederik Belien	Airbus Defense and Space	Germany
8		Sliding Mode Attitude Control of CubeSat with Magnetorquers	accepted	15'	withdrawn	Mr. Rasmus Holst	Aalborg University	Denmark
9		Dynamic analysis of thin-film solar panels in LEO	accepted	15'	confirmed	Ms. Laura Bettiol	University of Padova - DII	Italy
10		Quaternion-Based Leader-Following Attitude Coordination Control for Spacecraft Formation Flying	accepted	15'	no-show	Dr. Zhuo Zhang	Deep Space Exploration Research Center, Harbin Institute of Technology	China
11		Monte Carlo analysis of LIDAR-based pose calculation with respect to natural and artificial objects in the space environment	accepted	15'	withdrawn	Dr. John Woods	West Virginia University	United States
12		Impact of Atmospheric Perturbations on Tethered Satellite Systems	accepted	15'	withdrawn	Mr. Vishal Siewnarine	York University	Canada
13		Robust Backstepping Control of Magnetically Actuated Satellites with Unsymmetrical Mass Properties	accepted	15'	confirmed	Mr. Dipak Kumar Giri	Indian Institute of Technology	India