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Control moment Gyro gimble motor ultra-low velocity control system design with direct-drive PMSM

  • Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The advent of a Control Moment Gyro (CMG) system has a significant impact on the valid powerful torque output for a three axis attitude control of a spacecraft. The accurate torque of CMG output is mainly determined by the fluctuation of velocity of gimbal servo motor. In this paper, in order to achieve precise position of gimbal absolute position, the dual-channel rotating transformer is select. A velocity measurement method couple thick channel with thin channel is proposed. The feedback calibration of phase is proposed, which can great reduce nonlinear effect and weaken the parameter sensitive of gimbal servo system. The experiment results show that the velocity ratio can achieve 1:30000, and the lowest velocity can reach 1/10000rad/s.

Original languageEnglish
Title of host publicationProceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages2215-2219
Number of pages5
ISBN (Electronic)9781479925384
DOIs
StatePublished - 31 Aug 2015
EventInternational Conference on Mechatronics and Control, ICMC 2014 - Jinzhou, China
Duration: 3 Jul 20145 Jul 2014

Publication series

NameProceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014

Conference

ConferenceInternational Conference on Mechatronics and Control, ICMC 2014
Country/TerritoryChina
CityJinzhou
Period3/07/145/07/14

Keywords

  • Control Moment Gyro
  • Low Velocity Control
  • Rotating Transformer

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