Research on Modeling of the Agile Satellite Using a Single Gimbal Magnetically Suspended CMG and the Disturbance Feedforward Compensation for Rotors

The magnetically suspended Control Moment Gyroscope (CMG) has the advantages of long-life, micro-vibration and being non-lubricating, and is the ideal actuator for agile maneuver satellite attitude control. However, the stability of the rotor in magnetic bearing and the precision of the output torqu...

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Main Authors: Ning Yan, Peiling Cui
Format: Article
Language:English
Published: MDPI AG 2012-12-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/12/12/16964
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author Ning Yan
Peiling Cui
author_facet Ning Yan
Peiling Cui
author_sort Ning Yan
collection DOAJ
description The magnetically suspended Control Moment Gyroscope (CMG) has the advantages of long-life, micro-vibration and being non-lubricating, and is the ideal actuator for agile maneuver satellite attitude control. However, the stability of the rotor in magnetic bearing and the precision of the output torque of a magnetically suspended CMG are affected by the rapid maneuvers of satellites. In this paper, a dynamic model of the agile satellite including a magnetically suspended single gimbal control moment gyroscope is built and the equivalent disturbance torque effected on the rotor is obtained. The feedforward compensation control method is used to depress the disturbance on the rotor. Simulation results are given to show that the rotor displacement is obviously reduced.
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spelling doaj.art-1f16d5c40b4b4a7a9d76426e81b730582022-12-22T04:19:49ZengMDPI AGSensors1424-82202012-12-011212169641698710.3390/s121216964Research on Modeling of the Agile Satellite Using a Single Gimbal Magnetically Suspended CMG and the Disturbance Feedforward Compensation for RotorsNing YanPeiling CuiThe magnetically suspended Control Moment Gyroscope (CMG) has the advantages of long-life, micro-vibration and being non-lubricating, and is the ideal actuator for agile maneuver satellite attitude control. However, the stability of the rotor in magnetic bearing and the precision of the output torque of a magnetically suspended CMG are affected by the rapid maneuvers of satellites. In this paper, a dynamic model of the agile satellite including a magnetically suspended single gimbal control moment gyroscope is built and the equivalent disturbance torque effected on the rotor is obtained. The feedforward compensation control method is used to depress the disturbance on the rotor. Simulation results are given to show that the rotor displacement is obviously reduced.http://www.mdpi.com/1424-8220/12/12/16964Control Moment Gyroscopedynamic modelingfeedforward compensationmagnetic bearing
spellingShingle Ning Yan
Peiling Cui
Research on Modeling of the Agile Satellite Using a Single Gimbal Magnetically Suspended CMG and the Disturbance Feedforward Compensation for Rotors
Sensors
Control Moment Gyroscope
dynamic modeling
feedforward compensation
magnetic bearing
title Research on Modeling of the Agile Satellite Using a Single Gimbal Magnetically Suspended CMG and the Disturbance Feedforward Compensation for Rotors
title_full Research on Modeling of the Agile Satellite Using a Single Gimbal Magnetically Suspended CMG and the Disturbance Feedforward Compensation for Rotors
title_fullStr Research on Modeling of the Agile Satellite Using a Single Gimbal Magnetically Suspended CMG and the Disturbance Feedforward Compensation for Rotors
title_full_unstemmed Research on Modeling of the Agile Satellite Using a Single Gimbal Magnetically Suspended CMG and the Disturbance Feedforward Compensation for Rotors
title_short Research on Modeling of the Agile Satellite Using a Single Gimbal Magnetically Suspended CMG and the Disturbance Feedforward Compensation for Rotors
title_sort research on modeling of the agile satellite using a single gimbal magnetically suspended cmg and the disturbance feedforward compensation for rotors
topic Control Moment Gyroscope
dynamic modeling
feedforward compensation
magnetic bearing
url http://www.mdpi.com/1424-8220/12/12/16964
work_keys_str_mv AT ningyan researchonmodelingoftheagilesatelliteusingasinglegimbalmagneticallysuspendedcmgandthedisturbancefeedforwardcompensationforrotors
AT peilingcui researchonmodelingoftheagilesatelliteusingasinglegimbalmagneticallysuspendedcmgandthedisturbancefeedforwardcompensationforrotors