Data-driven model-free adaptive attitude control of partially constrained combined spacecraft with external disturbances and input saturation

Han GAO, Guangfu MA, Yueyong LYU*, Yanning GUO

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

40 Citations (Scopus)

Abstract

This study presents an improved data-driven Model-Free Adaptive Control (MFAC)strategy for attitude stabilization of a partially constrained combined spacecraft with external disturbances and input saturation. First, a novel dynamic linearization data model for the partially constrained combined spacecraft with external disturbances is established. The generalized disturbances composed of external disturbances and dynamic linearization errors are then reconstructed by a Discrete Extended State Observer (DESO). With the dynamic linearization data model and reconstructed information, a DESO-MFAC strategy for the combined spacecraft is proposed based only on input and output data. Next, the input saturation is overcome by introducing an anti-windup compensator. Finally, numerical simulations are carried out to demonstrate the effectiveness and feasibility of the proposed controller when the dynamic properties of the partially constrained combined spacecraft are completely unknown.

Original languageEnglish
Pages (from-to)1281-1293
Number of pages13
JournalChinese Journal of Aeronautics
Volume32
Issue number5
DOIs
Publication statusPublished - May 2019
Externally publishedYes

Keywords

  • Attitude control
  • Combined spacecraft
  • Data-driven control
  • Discrete Extended State Observer (DESO)
  • Input saturation

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