IAF Digital Library

5

session 5

Title: Attitude Dynamics - Part 1
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: 2011-10-05
Time: 15:00
Room: TS-04

IPC members

Chairman: Prof.Dr. Kazuya Yoshida, Tohoku University, Japan;
Chairman: Bang Hyochoong, Korea Advanced Institute of Science and Technology (KAIST), Korea, Republic of;
Rapporteur: Prof. Arun Misra, Mc Gill Institute for Aerospace Engineering (MIAE), Canada;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Research on coupled dynamics of large amplitude liquid sloshing with spacecraft based on 3d constraint surface model	15	confirmed	Dr. lei yang	China Academy of Space Technology (CAST)	China
2		A novel active controller for spin stabilized satellites using fluid rings	15	confirmed	Prof. Arun Misra	McGill University	Canada
3		Switched attitude control of an underactuated rigid satellite	15	confirmed	Mr. Lawrence Inumoh	Surrey Space Centre, University of Surrey	United Kingdom
4		Dynamics of a Rigid Multibody System with Loop Constrains using Only Independent Motion Variables	15	confirmed	Prof. Yinghong Jia	Beihang University	China
5		Precise Attitude Estimation of Solar Sail Spacecraft Utliziing Coupling between Attitude and Orbital dynamics	15	confirmed	Mr. kenji kitamura	Tokyo University	Japan
6		Analytical study of a three-stage magnetic attitude control to change a single-axis orientation	15	confirmed	Prof. Michael Yu Ovchinnikov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
7		A New Computer-Oriented Approach with Efficient Variables for Multibody Dynamics with Motion Constraints	15	confirmed	Mr. Quan Hu	Beihang University	China
8		Analysis on the Attitude Influence of Motions of Flexible Antennas and Attitude Control for Chinese TDRS	15	no-show	Dr. Xiaodong Han	China Academy of Space Technology (CAST)	China
9		Inertia-Free Attitude Control of Spacecraft with Unknown Time-Varying Mass Properties	15	confirmed	Mr. Avishai Weiss	University of Michigan	United States
10		Satellite attitude estimation by means of temperature measurements. Numerical approach	15	withdrawn	Prof. Maurizio Parisse	University of Rome “La Sapienza”	Italy
11		FEM-based evaluation of solar radiation pressure effect for spinning spacecraft	15	confirmed	Mr. Okano Yoshinobu	Tokyo Metropolitan University	Japan
12		robust and adaptive composite control of space flexible manipulator with bounded torque inputs based on the singular perturbation approach	15	no-show	Dr. Limin Xie	Fuzhou University	China