Computational Considerations for a Spacecraft Attitude Control System Employing Control Moment Gyros
Author:
Affiliation:
1. Texas A&M University, College Station, Texas
2. Southern Company Services, Inc., Birmingham, Ala.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57159
Reference30 articles.
1. Application of control moment gyros in the attitude control of the Apollo Telescope Mount
2. Stability analysis of the discrete-data Large-Space-Telescope system
3. On the general theory of control systems
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