IAF Digital Library

1

session 1

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: 2022-09-18
Time: 15:15
Room: S05

IPC members

Co-Chair: Prof. Giovanni B. Palmerini, Sapienza University of Rome, Italy;
Co-Chair: Prof. Robert G. Melton, Pennsylvania State University, United States;
Rapporteur: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	15:15	Design, realization and characterization of a free-floating platform for flexible satellite control experiments	15	confirmed	Dr. Marco Sabatini	Sapienza University of Rome	Italy
2	15:30	Reinforcement Learning for Attitude Control of a Spacecraft with Flexible Appendages	15	confirmed	Mr. Ahmed Mahfouz	University of Luxembourg	Luxembourg
3	15:45	reaction wheel unloading using external torque for variable shape spacecraft	15	confirmed	Mr. Yuki Amaki	Tokyo Institute of Technology	Japan
4	16:00	Fuzzy-Logic-Based Integrated Orbit-Attitude-Vibration Prescribed-Time Control for Large-Scale Flexible Spacecraft	15	confirmed	Dr. Chuang Liu	Northwestern Polytechnical University	China
5	16:15	Online policy iteration ADP-based control of post-capture combined spacecraft without inertia identifications	15	confirmed	Mrs. Jingyi Liu	Delft University of Technology (TU Delft)	The Netherlands
6	16:30	Attitude control of satellites with flexible appendages using inverse simulation	15	confirmed	Mr. Robert Gordon	University of Glasgow	United Kingdom
7	16:45	Time-Optimal Attitude Controller Design for Precision Pointing of an Agile Spacecraft using Deep Reinforcement Learning	15	confirmed	Dr. Vinod Kumar	Indian Space Research Organization (ISRO)	India
8	17:00	Invariant Sigma-Point Kalman Filtering on SO(3) for Attitude Estimation of a 3U CubeSat	15	confirmed	Mr. Joe Gibbs	School of Engineering, University of Glasgow	United Kingdom
9	17:15	Simultaneous Orbit-Attitude Control of Formation Flying Solar Sails around Sun-Earth L2 Using Reflectivity Modulation	15	confirmed	Mr. Keisuke Sugiura	Aoyama Gakuin University	Japan
10	17:30	Attitude Determination and Control System of the Student Small Satellite (SSS): An International Hands-On Satellite Project Among Asia Pacific Universities	15	confirmed	Ms. Niki Sajjad	K. N. Toosi University of Technology	Iran