Attitude Stabilization of a Spacecraft with Two Parallel Control Moment Gyroscopes
Author:
Affiliation:
1. York University, Toronto, Ontario M3J 1P3, Canada
2. Beihang University, 100191 Beijing, People’s Republic of China
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
http://arc.aiaa.org/doi/pdf/10.2514/1.G000982
Reference22 articles.
1. Control of Spacecraft Subject to Actuator Failures: State-of-the-Art and Open Problems
2. Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
3. Stabilization of Angular Velocity of Asymmetrical Rigid Body Using Two Constant Torques
4. Rate Damping of a Spacecraft Using Two Single-Gimbal Control Moment Gyros
5. Spin-axis stabilisation of underactuated rigid spacecraft under sinusoidal disturbance
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