IAF Digital Library

2

session 2

Title: Attitude Dynamics (2)
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: 2024-10-17
Time: 10:15
Room: Blue Hall 2

IPC members

Co-Chair: Prof. Toshio Kamiya, Meisei University, Japan;
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	10:15	Constrained rendezvous and mating with Gateway using nonlinear control techniques	15	confirmed	Dr. Mauro Pontani	Sapienza University of Rome	Italy
2	10:30	Elastic Oscillations of a Debris Removal Tether in an Inclined Towing Configuration	15	confirmed	Prof. Arun Misra	Mc Gill Institute for Aerospace Engineering (MIAE)	Canada
3	10:45	on-orbit experiment results on variable-shape satellite attitude dynamics using atmospheric drag torque and gravity gradient torque	15	confirmed	Mrs. Kiyona Miyamoto	Tokyo Institute of Technology	Japan
4	11:00	Simulation and experimental testing of an Iterative Learning Control strategy for Earth Observation attitude manoeuvres	15	confirmed	Dr. Federica Angeletti	University of Rome “La Sapienza”	Italy
5	11:15	Pointing Accuracy Using Model Predictive Control-based Guidance Control for DESTINY+ Flyby Mission	15	confirmed	Prof. Toshio Kamiya	Meisei University	Japan
6	11:30	Boresight Stabilization of an Axisymmetric Earth-pointing Satellite using Magnetorquers	15	confirmed	Prof. Fabio Celani	Sapienza University of Rome	Italy
7	11:45	Satellite Attitude Estimation with Hyperspectral Imaging for Autonomous Navigation	15	confirmed	Mr. Simão Marto	University of Strathclyde	United Kingdom
8	12:00	Design of flight control systems for RLVs with structural flexibility: application to the CALLISTO vehicle	15	confirmed	Mr. José Alfredo Macés-Hernández	German Aerospace Center (DLR), Bremen	Germany
9	12:15	Small Satellite Attitude Verification Using Multispectral Imagery of Moon and Earth Horizon Constellation	15	confirmed	Ms. Victoria Koßack	Technische Universität Berlin	Germany
10	12:30	adaptive prescribed performance attitude control for flexible spacecraft using observer	15	confirmed	Mr. Juhyeong Park	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of