On low-complexity control design to spacecraft attitude stabilization: An online-learning approach

Chengxi Zhang, Bing Xiao*, Jin Wu, Bo Li

*Corresponding author for this work

Research output: Contribution to journalJournal Articlepeer-review

23 Citations (Scopus)

Abstract

This paper studies the spacecraft attitude stabilization problem with external disturbances. A new control scheme entitled online-learning control is proposed to achieve a robust, accurate, and simple-structure control algorithm. Compared with the conventional control design, an obvious distinction of the online-learning control algorithm is that it together utilizes the previous control input information and the system's current state information, as if learning experience from previous control input. In contrast, the conventional control scheme does not fully use the existing information and chooses to discard the previous control input information when generating control instructions. Due to the learning strategy, the utility of adaptive- or observer-based tools can be avoided when designing a robust control law, making a simple, effective algorithm, moreover saving system resources. The proposed control law can stabilize the attitude system by achieving the uniformly ultimately bounded convergence.

Original languageEnglish
Article number106441
JournalAerospace Science and Technology
Volume110
DOIs
Publication statusPublished - Mar 2021
Externally publishedYes

Bibliographical note

Publisher Copyright:
© 2020 Elsevier Masson SAS

Keywords

  • Attitude stabilization
  • Online-learning control (OLC)
  • Spacecraft control

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