IAF Digital Library

3

session 3

Title: Attitude Dynamics
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: 2010-09-28
Time: 15:15
Room: North Hall

IPC members

Chairman: Prof. Andre Mazzoleni, North Carolina State University, United States;
Chairman: Bang Hyochoong, Korea Advanced Institute of Science and Technology (KAIST), Korea, Republic of;
Rapporteur: Prof. Fabio Santoni, Sapienza University of Rome, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Attitude Acquisition of Spacecraft with Multiple Liquid Stores	15	confirmed	Prof. Jay Kang	Korea Aerospace University	Korea, Republic of
2		Dynamics of Tethered Binary Asteroid Systems	15	confirmed	Prof. Andre Mazzoleni	North Carolina State University	United States
3		Efficient Attitude Control of Tether-Controlled Spinning Solar Sail using C.M.-C.P. Offset Torque and Virtual Structure Method	15	confirmed	Mr. Junichi Nishida	Tokyo Institute of Technology	Japan
4		Onboard Attitude Perturbation Estimation for Gyroless Spacecraft	15	confirmed	Prof. Steve Ulrich	Carleton University	Canada
5		Dynamic Control of Redundant Space Manipulators Suitable for Real-Time Applications	15	confirmed	Dr. Silvio Cocuzza	CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova	Italy
6		New Elements for the Efficient Propagation of Attitude Dynamics	15	confirmed	Dr. Martin Lara		Spain
7		Review and Analysis of Single-Thruster Attitude Control Algorithms for Spinning Spacecraft	15	confirmed	Mr. Robin Raus	EADS Astrium	United Kingdom
8		Singularity-Free Dynamic Equations of Spacecraft-Manipulator Systems	15	confirmed	Mr. Pål Johan From	Norwegian University of Science and Technology	Norway
9		Incremental Non-linear dynamic inversion control of a sounding rocket	15	withdrawn	Mr. A.L. Hertog	Delft University of Technology (TU Delft)	The Netherlands
10		Attitude Dynamics of a Pendulum-Shaped Charged Satellite	15	confirmed	Prof. Hiroshi Yamakawa	Kyoto University	Japan
11		Measurement and analysis of the solar array panel’s dynamic displacement caused by thermal snap using an on-board monitor camera	15	confirmed	Mr. Yusuke Hagiwara	Tokyo Institute of Technology	Japan
12		Lyapunov stability analysis of spacecraft attitude control system with control allocation	15	confirmed	Dr. Shengyong Tang	Harbin Institute of Technology	China