IAF Digital Library

5

session 5

Title: Attitude Dynamics (1)
type: oral
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 rigid and flexible bodies, including tethered systems, and in-orbit assembly.
Date: 2015-10-14
Time: 14:45
Room: Teddy B (ICC, lower level)

IPC members

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

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Natural periodic orbit-attitude behaviors for rigid bodies in three-body periodic orbits	15'	confirmed	Mr. Davide Guzzetti	Purdue University	United States
2		Attitude estimation and control design for single steerable single wing satellite	15'	confirmed	Dr. Hao-Chi Chang	National Space Organization	Taiwan, China
3		An efficient momentum dumping method through an alternative sun pointing strategy for small Near Equatorial Orbit satellite	15'	confirmed	Mr. Mihindukulasooriya Sheral Crescent Tissera	Nanyang Technological University	Singapore, Republic of
4		robust optimal sun-pointing control of a large solar power satellite	15'	withdrawn	Prof. Gianmarco Radice	University of Glasgow	United Kingdom
5		Nonlinear H-inf via Modified Rodrigues Parameters for Attitude Control in the Reuse of Retired Spacecraft Antenna	15'	confirmed	Mr. Xiaoyu Lang	Research Center of Satellite Technology, Harbin Institute of Technology	China
6		Attitude determination for the Unisat-6 microsatellite	15'	confirmed	Prof. Simone Battistini	Universidade de Brasília	Brazil
7		On the rotational Cucker-Smale model: optimal formation configuration and adaptive gains design	15'	confirmed	Mr. Fabrizio Paita	Universitat Politecnica de Catalunya (UPC)	Spain
8		multi-pendulum modeling of propellant sloshing via parameter optimization	15'	no-show	Mr. dong-yeon lee	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
9		coupled attitude-orbit dynamic modeling of high area-to-mass spacecraft and significance analysis of perturbation factors	15'	confirmed	Ms. Qiao Qiao	National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University	China
10		Determining High Rate Angular Velocity from Star Tracker Measurements	15'	confirmed	Prof. Fabio Curti	Sapienza - University of Rome	Italy
11		Adaptive Attitude Control for Spacecraft with Unknown Dead-Zone of Thruster	15'	no-show	Mr. LI DONGBAI	Research Center of Satellite Technology, Harbin Institute of Technology	China