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Nonlinear adaptive slewing motion control of spacecraft truss driven by synchronous V-gimbaled CMG precession

  • Di Zhou*
  • , Jingyang Zhou
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

The slewing motion control of a truss arm driven by a V-gimbaled control-moment-gyro (CMG) is a nonlinear control problem. The V-gimbaled CMG consists of a pair of gyros that must precess synchronously. The moment of inertia of the system, the angular momentum of the gyros and the external disturbances are not exactly known. With the help of feedback linearization and recursive Lyapunov design method, an adaptive nonlinear controller is designed to deal with the unknown items. Performance of the proposed controller is verified by simulation.

Original languageEnglish
Pages (from-to)332-338
Number of pages7
JournalChinese Journal of Aeronautics
Volume20
Issue number4
DOIs
StatePublished - Aug 2007

Keywords

  • Adaptive control
  • Attitude control
  • CMG
  • Feedback linearization
  • Synchronization

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