session 1

Title: Attitude Dynamics (1)
Description: This theme discusses advances in spacecraft attitude dynamics and control, as well as design, testing and performance of attitude sensors and actuators. This theme also covers dynamics and control of multiple interconnected rigid and flexible bodies, including tethered systems, and in-orbit assembly.
Date: 2013-09-23
Time: 15:15
Room: 306A

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		Maximum-Likelihood Estimation Optimizer for Constrained, Time-Optimal Satellite Reorientation	accepted	15'	confirmed	Prof. Robert G. Melton	Pennsylvania State University	United States
2		Drag-Free and Attitude Control for Chinese Planning ASTROD-I Mission	accepted	15'	confirmed	Ms. Yan Wei	Beihang University	China
3		Passive aerostability for drag sails	accepted	15'	confirmed	Mr. Andrew Wolahan	Cranfield University	The Netherlands
4		BRITE-Constellation: On-Orbit Attitude Performance of a Nanosatellite Telescope	accepted	15'	confirmed	Mr. Bryan Johnston-Lemke	Space Flight Laboratory, University of Toronto	Canada
5		Dynamic Decoupling of Slosh Motion in Thrusting Spacecraft with Multiple Large Liquid Stores	accepted	15'		Prof. Jay Kang	Korea Aerospace University	Korea, Republic of
6		UNIFORM ROTATIONS OF A TWO-BODY TETHERED SYSTEM IN AN ELLIPTIC ORBIT	accepted	15'	confirmed	Prof. Anna Guerman	Centre for Mechanical and Aerospace Science and Technologies (C-MAST)	Portugal
7		Hybrid Position/Force Control of Large Space manipulators	accepted	15'	confirmed	Dr. Dongming Ge	China Academy of Space Technology (CAST)	China
8		Design of spherical solar sails for spacecraft attitude maneuvers	accepted	15'	confirmed	Mr. Fedorenko Alexey	Moscow Institute of Electronics and Mathematics of National Research University Higher School of Economics (MIEM NRU HSE)	Russian Federation
9		Magnetic Attitude Control of a Two Body System in Drag Balance Instrument Implementation	accepted	15'	confirmed	Prof. Fabio Santoni	University of Rome “La Sapienza”	Italy
10		Discovering Razi acceleration via the theory of derivative kinematics and its application to the dynamic analysis of spacecraft systems	accepted	15'	confirmed	Mr. Ahmad Salahuddin Mohd Harithuddin	RMIT University (Royal Melbourne Institute of Technology)	Australia
11		finite-time continuous sliding mode magneto coulombic attitude control	accepted	15'	confirmed	Dr. Manoranjan Sinha	IIIT Kharagpur	India
12		A Nadir-Pointing Magnetic Attitude Control System for TigriSat nanosatellite	accepted	15'	confirmed	Mr. Paride Testani	Scuola Ingegneria Aerospaziale	Italy
13		Statistical research of the nanosatellite relative motion after separation from the rocket carrier upper stage	accepted	15'	confirmed	Prof. Igor V. Belokonov		Russian Federation