IAF Digital Library

8

session 8

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: 2021-10-29
Time: 09:45
Room: Sheikh Maktoum C

IPC members

Co-Chair: Dr. Shinji Hokamoto, Kyushu University, Japan;
Co-Chair: Prof. Giovanni B. Palmerini, Sapienza University of Rome, Italy;
Rapporteur: Prof. Robert G. Melton, Pennsylvania State University, United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	The LISA DFACS: effects of micro-meteoroid impacts in the drag-free mode	10	confirmed	Mr. Michele Pagone	Politecnico di Torino	Italy
2	09:55	Visual Servoing for Coordinated Precise Attitude Control in the TOM Small Satellite Formation	10	confirmed	Mr. Julian Scharnagl	Zentrum für Telematik	Germany
3	10:05	Attitude Dynamics and Operation Result in Hayabusa2 Capsule Reentry	10	confirmed	Mr. Kent Yoshikawa	Japan Aerospace Exploration Agency (JAXA)	Japan
4	10:15	magnetically controllable attitude trajectory constructed using the particle swarm optimization method	10	confirmed	Ms. Anna Okhitina	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
6	10:25	Determination and Mitigation of the Residual Magnetic Dipole Moment of CubeSats for Improved Attitude Stability	10	confirmed	Dr. Abdelmadjid Lassakeur	Agence Spatiale Algérienne (ASAL)	Algeria
7	10:35	Development and Analysis of a Pitch Sun Tracking Attitude Mode for the 2U CubeSat ORCASat	10	confirmed	Dr. Zeno Pavanello	University of Padova, DII / CISAS – “G. Colombo”	Italy
8	10:45	decentralised anti-windup fault tolerant control design for satellite attitude stabilization	10	confirmed	Mr. Ikechukwu Ofodile	Univeristy of Tartu	Estonia
1005	10:55	Real-Time Remaining Useful Life Prediction of Spacecraft Reaction Wheels Using Hybrid Model Based on Artificial Intelligence Techniques	10	confirmed	Dr. Krishna Kumar	Ryerson University	Canada
1009	11:05	unwinding and singularity free satellite attitude control using double-gimbal variable-speed control moment gyro and sliding control	10	confirmed	Ms. Gargi Das	Indian Institute of Technology Kharagpur	India
1010	11:15	A Fuel-Free and Agile Attitude Maneuver of Spinning Space Membrane Structures Using Electromagnetic Force	10	withdrawn	Mr. Yuki Yamada	Nagoya University	Japan
1011	11:25	Integrated Navigation Device for CubeSat Attitude Determination	10	withdrawn	Mr. Thu Vu Trong	Khalifa University of Science and Technology (KUST)	United Arab Emirates
1012	11:35	Attitude control of a nanosatellite using inverse simulation	10	confirmed	Mr. Robert Gordon	School of Engineering, University of Glasgow	United Kingdom
*		data-driven attitude robust control for microsatellite with an 1-D undeployed mechanism			Mr. Liming Fan	School of Astronautics, Beihang University	China
*		satellite attitude control using lorentz force generated by charge at low voltage		confirmed	Prof. Manoranjan Sinha	Indian Institute of Technology Kharagpur	India