Three-axis Attitude Control with Two Reaction Wheels and Magnetic Torquer Bars
Author:
Affiliation:
1. Johns Hopkins University
2. Orbital Sciences Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5245
Reference6 articles.
1. Overview of the [ITAL]Far Ultraviolet Spectroscopic Explorer[/ITAL] Mission
2. On-Orbit Performance of the [ITAL]Far Ultraviolet Spectroscopic Explorer[/ITAL] Satellite
3. Active Magnetic Damping Attitude Control for Gravity Gradient Stabilized Spacecraft
4. Linear Time-Varying Approach to Satellite Attitude Control Using Only Electromagnetic Actuation
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3. Hybrid Attitude Control for Nano-Spacecraft: Reaction Wheel Failure and Singularity Handling;Journal of Guidance, Control, and Dynamics;2021-03
4. Single-Axis Pointing of an Underactuated Spacecraft Equipped with Two Reaction Wheels;Journal of Guidance, Control, and Dynamics;2017-06
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