What is it about?
My publication is a method for stabilization of satellite with more accuracy in less time. Pyramidal Single Gimbal Control Moment Gyros are used for this system.
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Why is it important?
LQR/LQG method are used for controller in which the gimbal rates are selected as controller parameters. This linear method experimentally tested on nonlinear simulator.
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This page is a summary of: LQR/LQG attitude stabilization of an agile microsatellite with CMG, Aircraft Engineering and Aerospace Technology, March 2017, Emerald,
DOI: 10.1108/aeat-07-2014-0102.
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