IAF Digital Library

9

session 9

Title: Attitude Dynamics (2)
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: 13:30
Room: Sheikh Maktoum C

IPC members

Co-Chair: Prof. Gianmarco Radice, Singapore, Republic of;
Co-Chair: Prof. Toshio Kamiya, Meisei University, Japan;
Rapporteur: Dr. Zhanfeng Meng, China Academy of Space Technology (CAST), China;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	13:30	Exploiting Coriolis Acceleration to Reduce Libration Oscillations during Retraction of Tethered Satellite Systems	10	confirmed	Mr. Derek Bourabah	University at Buffalo	United States
2	13:40	Multi-Agent Attitude Task Allocation and Control in a Swarm of Magnetically Controlled CubeSats	10	confirmed	Mr. Ahmed Mahfouz	University of Luxembourg	Luxembourg
4	13:50	Implementation and testing of a passive magnetic attitude control system for the 3U AstroBio CubeSat orbiting in the Van Allen belt	10	confirmed	Dr. Stefano Carletta	Sapienza University of Rome	Italy
5	14:00	Three-Axis Attitude Control of Agile Satellite using Fractional Order Proportional-Derivative Controller	10	confirmed	Dr. Vinod Kumar	Indian Space Research Organization (ISRO)	India
6	14:10	Retrieval strategies for tethered satellites	10	confirmed	Mr. Alex Caon	CISAS "G. Colombo" - University of Padova	Italy
7	14:20	Attitude Determination and Control System of Sharjah-Sat-1	10	confirmed	Mr. Yousuf Faroukh	Sharjah Academy for Astronomy, Space Sciences and Technology (SAASST)	United Arab Emirates
8	14:30	Approaches to Optimal Control of Fluid-Dynamic Actuated Small Satellites	10	confirmed	Mr. Adrian Fried	Technische Universität Berlin	Germany
11	14:40	Attitude determination and control system testbed for hardware and software testing and validation for HYPSO small satellites	10	confirmed	Mr. Jørgen Anker Olsen	Norwegian University of Science and Technology	Norway
12	14:50	Effect of reaction wheels disbalances on the spacecraft stabilization accuracy	10	confirmed	Dr. Yaroslav Mashtakov	Keldysh Institute of Applied Mathematics of RAS	Russian Federation
1003	15:00	Dynamic Motion Planning For Satellite Attitude Maneuver Under Attitude Constrains Using Fuzzy Potential Field	10	confirmed	Mr. Fengwen Wang		China
1009	15:10	high precision satellite attitude control using double-gimbal variable-speed control moment gyro with unbalanced rotor	10	confirmed	Mr. Saumitra Barman	Indian Institute of Technology Kharagpur	India
1010	15:20	Attitude control of under-actuated satellite for ground moving target orientation	10	confirmed	Mr. ning cao	National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an,China	China
*		fault tolerant satellite attitude control using combined lorentz force and magnetic actuators		confirmed	Prof. Manoranjan Sinha	Indian Institute of Technology Kharagpur	India