IAF Digital Library

2

session 2

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: 2025-10-03
Time: 13:45
Room: Room C4.8

IPC members

Co-Chair: Dr. Krishna Dev Kumar, Toronto Metropolitan University, Canada;
Co-Chair: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;
Rapporteur: Bang Hyochoong, Korea Advanced Institute of Science and Technology (KAIST), Korea, Republic of;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	13:45	Optimal Bias-Momentum Control for Independently Tunable Spin Rate and Nutation Period	15	confirmed	Mr. Koki Kimura	Japan Aerospace Exploration Agency (JAXA), ISAS	Japan
2	14:00	UM5-EOSAT : In-orbit attitude determination and control system performance analysis and validation	15		Prof.Dr. Ilyas El Wafi		Morocco
3	14:15	controllability analysis and spin-axis pointing control of a non-cooperative satellite via laser ablation	15	confirmed	Ms. Yui Kawano	Kyushu University	Japan
4	14:30	Results of On-orbit Demonstration of Continuous Attitude Maneuver for Multi-point Earth Observation with Variable Shape Attitude Control Using Microsatellites HIBARI	15	confirmed	Mr. Ozeki Yusaku	Tokyo Institute of Technology	Japan
5	14:45	Control Strategies for Large Space Structures: Application to Orbiting Solar Reflectors	15	confirmed	Dr. Iain Moore	University of Glasgow	United Kingdom
6	15:00	Discrite-time large-angle attitude maneuver of spacecraft by reaction control system	15	confirmed	Dr. Yuichi Ikeda	Shonan Institute of Technology	Japan
7	15:15	Hierarchical Coordination-based Distributed Predefined-Time Stabilization for Multi-Arm Cooperative Control in Space Robotic Systems	15	confirmed	Mr. Lang Lu	Harbin Institute of Technology Shenzhen Graduate School	China
8	15:30	Advanced Spacecraft Simulation: High-Fidelity AOCS Simulation with CFD Integration and Flight data Validation	15	confirmed	Mr. Alessandro Visintini	OHB System AG-Bremen	Germany
9	15:45	Agile maneuvering control for a large non-contact satellite with flexible solar panels	15	confirmed	Dr. Zhuo Li	Shanghai Academy of Spaceflight Technology (SAST), China Aerospace and Technology Corporation (CASC)	China
10	16:00	attitude estimation using ai-based hyperspectral technology for autonomous close-proximity operations	15	confirmed	Mr. Alper Cakir	University of Strathclyde	United Kingdom