摘要
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.
| 源语言 | 英语 |
|---|---|
| 期刊论文编号 | 109378 |
| 期刊 | Aerospace Science and Technology |
| 卷 | 152 |
| DOI | |
| 出版状态 | 已出版 - 9月 2024 |
| 已对外发布 | 是 |
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