Adaptive neural network fault-tolerant control of hypersonic vehicle with immeasurable state and multiple actuator faults

Jun Wang, Cheng Zhang*, Chenming Zheng, Xinwan Kong, Jiayu Bao

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

11 Citations (Scopus)

Abstract

This paper proposes a fault-tolerant control scheme for tracking and controlling hypersonic vehicles with unknown dynamics, actuator failures, and unmeasurable states. The approach involves using a radial-based neural network to approximate the unknown dynamics and reconstruct the entire system model. Additionally, a neural network state observer is proposed to estimate the unmeasurable state of the system. To address the impact of actuator faults, a nonlinear observer is designed to estimate and compensate for the approximation error of the neural network system and fault values. Furthermore, a prescribed performance function is introduced to ensure both transient and steady-state performance of the system. The bounded stability of the closed-loop system is demonstrated through Lyapunov stability analysis.

Original languageEnglish
Article number109378
JournalAerospace Science and Technology
Volume152
DOIs
Publication statusPublished - Sept 2024
Externally publishedYes

Keywords

  • Actuator faults
  • Fault-tolerant control
  • Hypersonic flight vehicle
  • Prescribed performance control
  • Unmeasurable state

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