IAF Digital Library

6

session 6

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: 2019-10-24
Time: 09:45
Room: 150A

IPC members

Co-Chair: Dr. James O'Donnell, National Aeronautics and Space Administration (NASA), Goddard Space Flight Center, United States;
Co-Chair: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;
Rapporteur: Prof. Toshio Kamiya, Meisei University, Japan;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	Euclid Dark Universe Mission – High stability and pointing performance control	15	confirmed	Mr. Sergio Tiraplegui Riveras	SENER Ingenieria y Sistemas, S.A.	Spain
2	10:00	Analytic Spacecraft Attitude and Rate Estimation Performance During Attitude Sensor Outages	15	confirmed	Dr. Joseph Galante	NASA Goddard Space Flight Center Greenbelt MD 20771	United States
3	10:15	On the management of the satellite angular momentum taking advantage of external torques	15	confirmed	Ms. Sabrina Andiappane	Thales Alenia Space – France	France
4	10:30	Attitude Control for the LUMIO CubeSat in Deep Space	15	confirmed	Mr. Álvaro Romero-Calvo	Politecnico di Milano	Italy
5	10:45	Experimentation of Nonlinear Spacecraft Attitude Motion Control via Successive Linearization Based Model Predictive Control	15	confirmed	Mr. Burak Omer Iskender	Nanyang Technological University	Singapore, Republic of
6	11:00	Attitude Guidance and Control for Rapid Deorbit of Space Debris by Aerodynamic Drag	15	confirmed	Dr. Takahiro Sasaki	Japan Aerospace Exploration Agency (JAXA)	Japan
7	11:15	A Three-Axis Fluid-Dynamic Attitude Control Experiment for SALSAT	15	confirmed	Mr. Daniel Noack	Technische Universität Berlin	Germany
8	11:30	Analyzing the Stabilization of a Tumbling Satellite using Finite Element Methods	15	confirmed	Mr. Ryotaro SAKAMOTO	University of Colorado Boulder	United States
9	11:45	Coordinated Attitude Determination and Control in a Swarm of CubeSats	15	confirmed	Mr. Ahmed Mahfouz	Skolkovo Institute of Science and Technology	Russian Federation
10	12:00	ZERO PROPRLLANT MANEUVER PATH PLANNING OF SPACE SATTION UNDER MULTIPLE CONSTRAINTS	15	withdrawn	Mr. Zhuo Wang	Beijing Institute of Technology	China
11	12:15	Angular rate determination using star sensors and novel algorithms based on geometrical investigations	15	confirmed	Dr. Dario Spiller	Sapienza University of Rome	Italy
12	12:30	Sliding Mode Techniques for Precise Attitude Control	15	confirmed	Dr. Elisa Capello	Politecnico di Torino	Italy
*		Improved Magnetic Attitude Control		confirmed	Mr. Mohammed Desouky	Michigan Technological University	United States
*		Rapid Functional Verification of Attitude Control Algorithms on a Spacecraft Motion Platform with Control Moment Gyroscopes			Mr. Simon Goerries	Airbus Defence and Space	Germany