IAF Digital Library

1

session 1

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: 2023-10-03
Time: 15:00
Room: BCC B4

IPC members

Co-Chair: Prof. Giovanni B. Palmerini, Sapienza University of Rome, Italy;
Co-Chair: Dr. Zhanfeng Meng, China Academy of Space Technology (CAST), China;
Rapporteur: Prof. Robert G. Melton, Pennsylvania State University, United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	15:00	Absolute Visual Servoing for Precise Earth Target Pointing Onboard Small Satellites	15	confirmed	Mr. Ilham Mammadov	Zentrum für Telematik	Germany
2	15:15	Pointing Stability of HiZ-GUNDAM Satellite After Agile Attitude Maneuvers Under the Rate Bias Error of Fiber Optic Gyros	15	confirmed	Prof. Toshio Kamiya	Meisei University	Japan
3	15:30	Deep reinforcement learning-based gain scheduling for attitude control of microsatellites with changing inertia	15	withdrawn	Mr. Joe Gibbs	School of Engineering, University of Glasgow	United Kingdom
4	15:45	Optimal Attitude Path Planning Along Torque Equilibrium Points Using Aerodynamic Database for Deorbiting Large Debris by Small Satellites	15	confirmed	Dr. Takahiro Sasaki	Japan Aerospace Exploration Agency (JAXA)	Japan
5	16:00	Multi-objective Optimization of Attitude Maneuver Planning for Flexible Asteroid Lander Using Population Evolutionary Algorithm	15		Mr. Zhe Zhu	Beijing Institute of Technology	China
6	16:15	The effects of pointing error sources on energy delivery from orbiting solar reflectors	15	confirmed	Dr. Iain Moore	University of Glasgow	United Kingdom
7	16:30	A Free-Floating 3-axis Attitude Control Test Environment with Optical Tracking for High-Precision Pointing Verification of CubeSats	15	confirmed	Mr. Ilham Mammadov	Zentrum für Telematik	Germany
8	16:45	Liquid-filled spacecraft finite-time attitude maneuver control with angular and velocity constraint	15	confirmed	Ms. Wei Zhang	School of Astronautics, Harbin Institute of Technology	China
9	17:00	Attitude Dynamics of Small Satellites in Circular Near-Equatorial LEO/VLEO	15	confirmed	Dr. Dmitry A. Sizov	Nazarbayev University	Kazakhstan
10	17:15	Prescribed Performance Adaptive Control with Fault-tolerance Capability for a Sun-pointing Spacecraft on Halo Orbit	15	confirmed	Mr. Srianish Vutukuri	Indian Institute of Science	India