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: 2026-10-05
Time: 16:30
Room: Hall 8

IPC members

Co-Chair: Prof. Marcello Romano, Technical University of Munich (TUM), Germany;
Co-Chair: Prof. Bin Meng, Beijing Institute of Control Engineering, Beijing, 100080, P.R. China, China;
Rapporteur: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	16:30	CABLESSail: Momentum Management Actuator for Next-Generation Solar Sails	15	confirmed	Ms. Soojeong Lee	University of Minnesota Twin Cities	United States
2	16:45	In-Orbit Demonstration and Efficient Use of the Garriott – Dzhanibekov Effect in the ANSER Cluster	15	confirmed	Mr. Cesar Arza	Instituto Nacional de Tecnica Aeroespacial (INTA)	Spain
3	17:00	Autonomous Multi-Mode GNC for VLEO CubeSats: Monte Carlo Validation of High-Rate Deployment Recovery and Precision Pointing	15	confirmed	Mr. Batuhan Akkova		Türkiye
4	17:15	Three-Axis Attitude Control and Vibration Suppression \\ for Spacecraft with Flexible Structures: \\ An Approach Using Decoupled Optimal Servo Control (DECOPS)	15	confirmed	Mr. Yuto Yamamoto	Osaka Metropolitan University	Japan
5	17:30	Active Feedback Control of Electrodynamic Tethers in LEO: Mitigating Kinematic Instability via CubeSat Swarm Logic and Tension Modulation	15	confirmed	Mr. Muhammad Teymurlu	Baku Higher Oil School	Azerbaijan
6	17:45	Data-Driven Takeover Control for Non-Cooperative Spacecraft with Unknown Parameters: Design and Experimental Validation	15	confirmed	Dr. Ziyu Yang	Northwestern Polytechnical University;National Key Laboratory of Aerospace Flight Dynamics	China
7	18:00	Dioscuri: A Dual–Solar-Array Cooperative Momentum Unloading System	15	confirmed	Dr. Changgang Zheng	Institute of Spacecraft System Engineering,China Academy of Space Technology (CAST)	China
8	18:15	Stable Reinforcement Learning–Based Spacecraft Attitude Control with Magnetic-Only Actuation	15	confirmed	Prof. Fabio Curti	University of Arizona	United States
9	18:30	On-Orbit Demonstration of Multi-Point Earth Observation Enabled by Variable-Shape Attitude Control with Ground Pointing Estimation during Rapid Maneuvers on the Microsatellite HIBARI	15	confirmed	Mr. Yusaku Ozeki	Tokyo Institute of Technology	Japan
10	18:45	Stabilization of the Orbital Orientation of a Spacecraft Using a System of Momentum Control Devices	15	confirmed	Ms. Eva Kolomiets	Bauman Moscow State Technical University	Russian Federation