Observer-based sliding mode fault-tolerant control for spacecraft attitude system with actuator faults

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Abstract

The paper investigate the fault-tolerant attitude control for the rigid spacecraft attitude system with external disturbances and actuator faults simultaneously. Firstly, an iterative learning-based observer is proposed, which can estimate the actuator faults with high precise even in presence of the disturbance. Then, employing the estimate informations of the designed observer, a sliding-mode fault-tolerant control scheme is designed to guarantee stability of the closed-loop system and reject to the external disturbance. Finally, the simulation results are given to validate the effectiveness of the proposed approaches.

Original languageEnglish
Title of host publicationProceedings of 2019 11th CAA Symposium on Fault Detection, Supervision, and Safety for Technical Processes, SAFEPROCESS 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages154-159
Number of pages6
ISBN (Electronic)9781728106816
DOIs
StatePublished - Jul 2019
Event11th CAA Symposium on Fault Detection, Supervision, and Safety for Technical Processes, SAFEPROCESS 2019 - Xiamen, China
Duration: 5 Jul 20197 Jul 2019

Publication series

NameProceedings of 2019 11th CAA Symposium on Fault Detection, Supervision, and Safety for Technical Processes, SAFEPROCESS 2019

Conference

Conference11th CAA Symposium on Fault Detection, Supervision, and Safety for Technical Processes, SAFEPROCESS 2019
Country/TerritoryChina
CityXiamen
Period5/07/197/07/19

Keywords

  • Actuator faults
  • Fault-tolerant control
  • Observer
  • Spacecraft attitude system

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