IAF Digital Library

9

session 9

Title: Attitude Dynamics (2)
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: 2016-09-30
Time: 13:30
Room: Salon Jalisco E6

IPC members

Co-Chair: Dr. James O'Donnell, National Aeronautics and Space Administration (NASA), Goddard Space Flight Center, United States;
Co-Chair: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;
Rapporteur: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Periodic orbit-attitude solutions along planar orbits in a perturbed circular restricted three-body problem for the Earth-Moon system	15'	confirmed	Mr. Lorenzo Bucci	Politecnico di Milano	Italy
2		Orbit-attitude Coupled Motion around Small Bodies: Sun-synchronous Orbits with Sun-tracking Attitude Motion	15'	confirmed	Mr. Shota Kikuchi	University of Tokyo	Japan
3		A Fluid-Dynamic Attitude Control System for TechnoSat	15'	withdrawn	Mr. Daniel Noack	Technische Universität Berlin	Germany
4		Capturing and Docking Spacecraft with Flux Pinned Interfaces	15'	confirmed	Ms. Frances Zhu	Cornell University	United States
5		Star Tracker Performance during the Early Phases of the Lisa Pathfinder Mission	15'	confirmed	Dr. Jonathan Grzymisch	European Space Agency (ESA-ESTEC)	The Netherlands
6		Fractional PID Control of Spacecraft Attitude Dynamics using Rotation Matrices	15'	confirmed	Prof. Eric Butcher	University of Arizona	United States
7		Gain-Scheduled Attitude Control with Power Tracking and Singularity Avoidance of Double-Gimbal Variable-Speed Control Moment Gyros	15'	confirmed	Mr. Takahiro Sasaki	Osaka Prefecture University	Japan
8		Operations in space of SPACESTAR: the new star tracker for future recurrent platforms	15'	confirmed	Mr. FRANCO BOLDRINI	Leonardo S.p.A	Italy
9		The control of space tethered system	15'	withdrawn	Dr. Alexey Malashin	Moscow State University	Russian Federation
10		Long term passive attitude stabilisation using radiation torques	15'	withdrawn	Dr. Stuart Grey	University College London (UCL)	United Kingdom
11		Dual tensor solution to the extended Wahba problem	15'	confirmed	Prof. Daniel Condurache	Technical University of Iasi	Romania
12		design and validation of the attitude control system for three-axis stabilized nano-satellites	15'	withdrawn	Mr. Dechao Ran		China
13		Motion Prediction of Non-Cooperative Target Based on Autoregressive Model	15'	confirmed	Dr. Mingming Wang	Northwestern Polytechnical University	China