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: 2025-10-03
Time: 10:15
Room: Room C4.8

IPC members

Co-Chair: Dr. Marcello Romano, Technical University of Munich, Germany;
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	10:15	Autonomous Magnetic Attitude Control of Resource-Constrained Femtosatellites	15		Mr. Satyam Bhatti	University of Glasgow	United Kingdom
2	10:30	A Geometric Approach to Near-Optimal Feedback Spacecraft Reorientation with Exclusion Cones	15		Dr. Mauro Pontani	Sapienza University of Rome	Italy
3	10:45	Technology for attitude reconstruction of a LEO nanosatellite on the example of SamSat-Ionosphere	15		Prof. Igor V. Belokonov	Samara National Research University (Samara University)	Russian Federation
4	11:00	Robust Attitude Estimation for Nanosatellites with Deployable Panels Shadowing the Sun Sensors	15		Mr. Mehmet Esit	Kyushu Institute of Technology	Japan
5	11:15	LQR Attitude Control Design for an On-Orbit Assembled Spacecraft	15		Mr. David Bacher	Viterbi School of Engineering, USC	United States
6	11:30	Development of Adaptive Control and Center-of-Mass Estimation Laws with Concurrent Learning Modifications for a 3-degree-of-freedom Spacecraft Testbed	15		Mr. Pol Fontdegloria Balaguer	Embry-Riddle Aeronautical University	United States
7	11:45	Energy-optimal Attitude Control of Ultra-large-scale Spacecraft: An Off-policy Actor-critic Approach	15		Ms. Jieyu Zhang	Harbin Institute of Technology	China
8	12:00	VEKTOR-FDA: Advancements in the Development and Implementation of a Fluid Dynamic Attitude Control Actuator with Multiple Degrees of Freedom Based on Liquid Metal for Small Satellites	15		Mr. Huu Quan Vu	Technical University of Berlin	Germany
9	12:15	Chaotic attitude motion of aerodynamically stabilized magnetic satellites with dampers in elliptical polar Earth orbits	15		Dr. Dmitry A. Sizov	Nazarbayev University	Kazakhstan
10	12:30	On-Orbit Experiment of Angular Momentum Control by External Torque Changes Using Variable Shape Function	15		Mr. Yuki Amaki	Tokyo Institute of Technology	Japan
1*	10:15	Comparative analysis of robust and predictive control approaches for sounding rocket attitude control	15		Ms. Natalia Wiśniewska	Poznan University of Technology	Poland
2*	10:30	Development of a Control and Prediction Method for the Attitude of a 3.5 U CubeSat Optimized with Artificial Neural Networks for Sustainable Use in Low-Earth Orbit Missions	15	confirmed	Mr. Kevin Stib Cardenas Rosales	Universidad Nacional de Ingenieria, Peru	Peru
3*	10:45	Calibration and Precise Attitude Determination \\ Process for MUP Satellite	15		Mrs. Sirin Yakupoglu Altuntas	TAI - Turkish Aerospace Industries, Inc	Türkiye
4*	11:00	Passive stabilization using magnetorquers on a 1U student CubeSat	15		Mr. Simone Ceola	Politecnico di Milano	Italy