Adaptive output feedback attitude control for reusable launch vehicle with input constraints and actuator faults

  • Wenting Li
  • , Jinsong Zhao
  • , Shanwei Su*
  • , Ran Mo
  • , Yan Lin
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

This paper considers an adaptive output feedback fault tolerant control (FTC) for a reusable launch vehicle (RLV) during reentry phase for which four grid fins are used as actuators. Based on a prescribed tracking performance and an auxiliary system to deal with the input constraints, the proposed adaptive controller can compensate for the effect of uncertainties, external and internal disturbances, input constraints and actuator faults. It is shown that with the proposed scheme, the system tracking performance can be guaranteed even in the presence multiple actuator faults. The influence of the input constraints on the tracking performance is also investigated. Simulation results are presented to illustrate the effectiveness of the proposed scheme.

Original languageEnglish
Article number108616
JournalAerospace Science and Technology
Volume142
DOIs
StatePublished - Nov 2023

Keywords

  • Backstepping control
  • Fault tolerant control
  • Prescribed transient
  • Reusable launch vehicle
  • Steady state performance

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