IAF Digital Library

1

session 1

Title: Attitude Dynamics (1)
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: 2024-10-16
Time: 15:00
Room: Blue Hall 2

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	Attitude Control in Wheel Reduction Operation of Hayabusa2 Extended Mission	15	confirmed	Mr. Takefumi Kosaka	NEC Corporation	Japan
2	15:15	Model Predictive Control for underactuated spacecraft equipped with two reaction wheels in the presence of a residual angular momentum	15	confirmed	Prof. Giulio Avanzini	Università del Salento	Italy
3	15:30	Gravity gradient effects on the attitude dynamics on satellites in Near-Rectilinear Halo Orbits	15	confirmed	Dr. Erica Scantamburlo	Politecnico di Torino	Italy
4	15:45	Real-time attitude control for optimal low-thrust multi-revolution coplanar transfers	15	confirmed	Dr. Stefano Carletta	Sapienza University of Rome	Italy
5	16:00	Agile attitude control of variable-shape spacecraft with reduced time delay	15	confirmed	Dr. Kei Watanabe	Tokyo Institute of Technology	Japan
6	16:15	Study of attitude determination accuracy and Earth-point stabilization performance using asynchronous star tracker and angular velocity sensor measurements	15	confirmed	Dr. Danil Ivanov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
7	16:30	Analysis method and research of contact collision process based on attitude evolution of fast tumbling target in space	15	confirmed	Ms. Jiale Chen	Northwestern Polytechnical University;National Key Laboratory of Aerospace Flight Dynamics	China
8	16:45	A causal learning approach to in-orbit inertial parameter estimation for multi-payload deployers.	15	confirmed	Mr. Konstantinos Platanitis	Cranfield University, UK	United Kingdom
9	17:00	GYSELE : an attitude estimation and non-stellar object tracking system	15	confirmed	Mr. Etienne Perot	Centre National d'Etudes Spatiales (CNES)	France
10	17:15	Control of external directional exposures of various surface locations on the tumbling spacecraft using "Inertial Morphing"	15	confirmed	Prof. Pavel M. Trivailo	RMIT University, Australia	Australia