Technical Papers
Jul 25, 2016

Composite Adaptive Control of Single Gimbal Control Moment Gyroscope Supported by Active Magnetic Bearings

Publication: Journal of Aerospace Engineering
Volume 30, Issue 1

Abstract

In this work, a control moment gyroscope (CMG) supported by active magnetic bearing (AMB) is considered with a gimbal angular movement. Gimbal angular movement in a CMG imposes extra load on magnetic bearings. A complete model of the CMG system with flywheel, AMBs, and gimbal dynamics is derived for control design. Lyapunov based composite adaptive output feedback control is proposed for fast uncertainty compensation in the CMG system, and some simulation results are presented. For a gimbal angular velocity input, a flywheel rotor magnetic bearing system is simulated at constant rotational speed of the flywheel rotor.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 30Issue 1January 2017

History

Received: Nov 9, 2015
Accepted: May 23, 2016
Published online: Jul 25, 2016
Discussion open until: Dec 25, 2016
Published in print: Jan 1, 2017

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Authors

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Sinan Basaran [email protected]
Research Assistant, Dept. of Mechanical Engineering, Gebze Technical Univ., Gebze 41400, Turkey. E-mail: [email protected]
Selim Sivrioglu [email protected]
Professor, Dept. of Mechanical Engineering, Gebze Technical Univ., Gebze 41400, Turkey (corresponding author). E-mail: [email protected]
Erkan Zergeroglu [email protected]
Associate Professor, Dept. of Computer Engineering, Gebze Technical Univ., Gebze 41400, Turkey. E-mail: [email protected]

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