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Steering Law of Control Moment Gyros for Reducing Singularity Measure Conservativeness

  • Harbin Institute of Technology
  • Aerospace System Engineering Shanghai

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

Abstract

The two main types of real-time computational steering laws of control moment gyros (CMG), including null motion and singular robust (SR) inverse methods, have their deficiencies and limitations. A novel steering law is proposed to reduce further the conservativeness of singularity measure based on gimbal angle combination. Based on SR steering logics, the angle between commanded control torque and the singular vector is considered to determine the magnitude of the introduced error, thereby reducing the unnecessary torque error. And by introducing an additional term in the gimbal rate command, the CMG cluster is always driven to track the desired torque as much as possible. Several numerical simulations including comparisons with existing steering laws are presented to demonstrate the feasibility and effectiveness of the proposed algorithm.

Original languageEnglish
Title of host publicationProceedings - 2019 Chinese Automation Congress, CAC 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages2145-2150
Number of pages6
ISBN (Electronic)9781728140940
DOIs
StatePublished - Nov 2019
Event2019 Chinese Automation Congress, CAC 2019 - Hangzhou, China
Duration: 22 Nov 201924 Nov 2019

Publication series

NameProceedings - 2019 Chinese Automation Congress, CAC 2019

Conference

Conference2019 Chinese Automation Congress, CAC 2019
Country/TerritoryChina
CityHangzhou
Period22/11/1924/11/19

Keywords

  • Attitude maneuver
  • control moment gyroscope
  • singularity measure
  • steering law

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