Magnetic Attitude Control of a Flexible Satellite

Author:

Findlay Everett J.1,Ruiter Anton de2,Forbes James R.3,Liu Hugh H. T.1,Damaren Christopher J.1,Lee James4

Affiliation:

1. Institute for Aerospace Studies, University of Toronto, Toronto, Ontario M3H 5T6, Canada

2. Department of Aerospace Engineering, Ryerson University, Toronto, Ontario M5B 2K3, Canada

3. Department of Mechanical Engineering and Centre for Intelligent Machines, McGill University, Montreal, Quebec H3A 0C3, Canada

4. Space Science and Technology, Canadian Space Agency, Saint-Hubert, Quebec J3Y 8Y9, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

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1. Adaptive Sliding Mode Variable Structure Attitude Control for Space Robot;2024 IEEE 7th Advanced Information Technology, Electronic and Automation Control Conference (IAEAC);2024-03-15

2. Magnetic Control Law with Controlled Rotation Rate for Dual Spin Satellite;Journal of Guidance, Control, and Dynamics;2024-02-29

3. Attitude Control of Magnetically Actuated Satellite in Circular Orbit: A Controllability Analysis;AIAA SCITECH 2024 Forum;2024-01-04

4. Overview;Advanced Attitude Control of Satellite;2024

5. Attitude control experiment of a spinning spacecraft using only magnetic torquers;Advances in Space Research;2023-06

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