session 2

Title: Attitude Dynamics (2)
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: 2013-09-24
Time: 09:45
Room: 306A

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		LONG TERM DYNAMICS AND CONTROL OF A BARE ELECTRODYNAMIC TETHERS UNDER MULTI-ENVIRONMENT PERTURBATIONS	accepted	15'	confirmed	Dr. Rui Zhong	York University	China
2		Research on Design and Performance Analysis of High Power Electromechanical Actuator Applied to Spacecrafts	accepted	15'	confirmed	Dr. yuexuan wang	China Academy of Launch Vehicle Technology (CALT)	China
3		experimental demonstration of 3-dof capabilities of a tilted wheel using an air-bearing table	accepted	15'	confirmed	Mr. Lawrence Inumoh	Surrey Space Centre, University of Surrey	United Kingdom
4		A residual-based Adaptive Unscented Kalman Filter for microsatellites	accepted	15'	confirmed	Dr. Le Xuan Huy	Tokyo Institute of Technology	Vietnam
5		ANALYSIS AND EXPERIMENTS FOR DELAY COMPENSATION IN ATTITUDE CONTROL OF FLEXIBLE SPACECRAFT	accepted	15'	confirmed	Dr. Marco Sabatini	Sapienza University of Rome	Italy
6		observer-based robust sliding mode control for spacecraft attitude maneuver subject to reaction wheel friction	accepted	15'	confirmed	Dr. Shunan Wu	Dalian University of Technology (DUT)	China
7		Determination of spacecraft inertial parameters on board.	accepted	15'	withdrawn	Mr. Dmitry Timoshin	TSNIIMASH	Russian Federation
8		two stage de-tumbling for twin nano-satellites studsat-2a/2b	accepted	15'	confirmed	Mr. Saroj Kumar	Nitte Meenakshi Institute Of Technology.	India
9		Joint-Space Dynamics Algorithm of Space Manipulators with Tree Structure by Using Inertia Mapping Matrix	accepted	15'	confirmed	Mr. Mingming Wang	Technical University of Munich	Germany
10		Spacecraft Sun Pointing Using Coplanar Solar Panels Data and Magnetic Field Measurements	accepted	15'	confirmed	Dr. Mohammad Abdelrahman	International Islamic University Malaysia	Malaysia
11		Control algorithms development for space platform with a rotating solar sail	accepted	15'	confirmed	Mr. Aleksandr Zykov	S.P. Korolev Rocket and Space Corporation Energia	Russian Federation
12		a method of guide star selection for star identification in the condition of high background and high dynamic	accepted	15'	confirmed	Dr. Wei Zhang	China Aerospace Science and Industry Corporation	China
13		robust sliding mode control of a moving-mass actuated suborbital reentry biological payload	accepted	15'	confirmed	Mr. Aidin Mohammadi	Aerospace Research Institute	Iran