IAF Digital Library

5

session 5

Title: Attitude Dynamics (1)
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: 2019-10-23
Time: 14:45
Room: 150A

IPC members

Co-Chair: Dr. Shinji Hokamoto, Kyushu University, Japan;
Co-Chair: Prof. Gianmarco Radice, Singapore, Republic of;
Rapporteur: Prof. Giovanni B. Palmerini, Sapienza University of Rome, Italy;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	14:45	SWOT: an AOCS answering to high payload constraints	15	confirmed	Mr. Bertrand RAFFIER	Centre National d'Etudes Spatiales (CNES)	France
2	15:00	Impact of Strain-Actuated Attitude Control Systems for Variant Mission Classes	15	confirmed	Mr. FNU Vedant	University of Illinois	United States
3	15:15	on the attitude control by thruster of a spinning solar sail and bending moment's effect analysis	15	confirmed	Mr. Roger Bertran Rabat	Department of Engineering, The University of Tokyo	Spain
4	15:30	Semi-analytical Approach to Fasten Complex and Flexible Pointing Strategies Definition for Nanosatellite Clusters: the HERMES Mission Case from Design to Flight	15	confirmed	Mr. Jacopo Prinetto	Politecnico di Milano	Italy
5	15:45	Detumbling and Attitude Control of Cubesats via Multi-Model Based Embedded Optimization	15	confirmed	Mr. Wee Meng Ng	THALES GROUP	Singapore, Republic of
6	16:00	Model Predictive Steering Control Law for Double-gimbal Scissored Pairs of Control Moment Gyros	15	confirmed	Prof. Hirohisa Kojima	Tokyo Metropolitan University	Japan
7	16:15	Control of an Over-Actuated Spacecraft using a Combination of a Fluid Actuator and Reaction Wheels	15	confirmed	Dr. Sebastian Grau	Technische Universität Berlin	Germany
8	16:30	Forward Dynamics Algorithm for Origami-Folded Deployable Spacecraft Structures	15	confirmed	Ms. JoAnna Fulton	University of Colorado Boulder	United States
9	16:45	Coupled Motion Determination and Stabilization of a Satellite Equipped with Large Flexible Elements Using ADCS Only	15	confirmed	Dr. Danil Ivanov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
10	17:00	minimum jerk attitude slew maneuvers	15	withdrawn	Mr. Arland Thompson	Raytheon	United States
11	17:15	Design and Hardware-in-the-Loop Test of an Active Magnetic Detumbling and Pointing Control based only on Three-Axis Magnetometer Data	15	confirmed	Mr. Stefano Carletta	Sapienza University of Rome	Italy
12	17:30	experimental validation of agile attitude control with sinc function-based profiler for reducing residual vibrations	15	confirmed	Dr. Toshio Kamiya	NEC Corporation	Japan