Optimal Gyricity Distribution for Space Structure Vibration Control
Author:
Affiliation:
1. Department of Mechanical Engineering, McGill University, Montreal, Quebec H3A 0C3, Canada
2. Institute for Aerospace Studies, University of Toronto, Toronto, Ontario M3H 5T6, Canada
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.G000293
Reference24 articles.
1. Lecture Notes in Mathematics;Bensoussan A.,1972
2. AubrunJ. N.MarguliesG. “Gyrodampers for Large Space Structures,” NASA CR-159171, Feb. 1979.
3. Scissored-Pair Control-Moment Gyros: A Mechanical Constraint Saves Power
4. Control Law for Active Structural Damping Using a Control Moment Gyro
5. A COMPARISON OF THE EFFECTIVENESS OF DOUBLE- AND SINGLE-GIMBALED CONTROL MOMENT GYROSCOPES FOR VIBRATION SUPPRESSION
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