Adaptive Singularity-Free Control Moment Gyroscopes
Author:
Affiliation:
1. Akrobotix LLC, Syracuse, New York 13202
2. Syracuse University, Syracuse, New York 13244
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.G003545
Reference18 articles.
1. Torque amplification of control moment gyros
2. WieB. (ed.), Space Vehicle Dynamics and Control, Revised 1st ed., AIAA, Reston, VA, 2015, pp. 436–437. doi:10.2514/4.103803
3. SchaubH.JunkinsJ. L., Analytical Mechanics of Space Systems, 4th ed., AIAA, Reston, VA, 2018, pp. 150–151. doi:10.2514/4.105210
4. KurokawaH. “A Geometric Study of Single Gimbal Control Moment Gyros (Singularity Problems and Steering Law),” Tech. Rept. 175, Agency of Industrial Technology and Science, Mechanical Engineering Lab., Japan, 1998.
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