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	Scaling and Nondimensionalization of the Rotational Mechanics of a Rigid Body Spacecraft	15		Dr. Marcello Romano	Technical University of Munich	Germany
3	14:15	controllability analysis and spin-axis pointing control of a non-cooperative satellite via laser ablation	15		Ms. Kawano Yui	Kyushu University	Japan
4	14:30	Protein-inspired reconfiguration strategy for hinge-connected modular spacecraft	15		Prof.Dr. Ti Chen	Nanjing University of Aeronautics and Astronautics	China
5	14:45	Control Strategies for Large Space Structures: Application to Orbiting Solar Reflectors	15		Dr. Iain Moore	University of Glasgow	United Kingdom
6	15:00	Discrite-time large-angle attitude maneuver of spacecraft by reaction control system	15		Dr. Yuichi Ikeda	Shonan Institute of Technology	Japan
7	15:15	Spin-Momentum Tracking Orbit Normal with Thruster Pulses – Bhaskara Satellite Revisited	15		Prof. Hari Hablani	Indian Institute of Technology	India
8	15:30	Advanced Spacecraft Simulation: High-Fidelity AOCS Simulation with CFD Integration and Flight data Validation	15		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		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		Mr. Alper Cakir	University of Strathclyde	United Kingdom
1*	13:45	UM5-EOSAT : In-orbit attitude determination and control system performance analysis and validation	15		Prof.Dr. Ilyas El Wafi		Morocco
2*	14:00	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
3*	14:15	Hierarchical Coordination-based Distributed Predefined-Time Stabilization for Multi-Arm Cooperative Control in Space Robotic Systems	15		Mr. Lang Lu	Harbin Institute of Technology Shenzhen Graduate School	China