Single-Axis Pointing of an Underactuated Spacecraft Equipped with Two Reaction Wheels
Author:
Affiliation:
1. University of Rome “La Sapienza”, 00184 Rome, Italy
2. University of Bologna, 47121 Forl, Italy
3. University of Salento, 73100 Lecce, Italy
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
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G002182
Reference10 articles.
1. Three-axis Attitude Control with Two Reaction Wheels and Magnetic Torquer Bars
2. Constrained Slews for Single-Axis Pointing
3. Spin-axis stabilization of symmetric spacecraft with two control torques
4. Spin-Axis Stabilization of a Rigid Spacecraft Using Two Reaction Wheels
5. A novel approach to the attitude control of axisymmetric spacecraft
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3. Backstepping-Based Steering Control for Spacecraft Attitude Control Using Two-Skewed Control Moment Gyroscopes;Journal of Guidance, Control, and Dynamics;2023-01
4. Spin Axis Control Using Reaction Wheels: Modeling and Experimental Validation;Journal of Aerospace Engineering;2022-09
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