摘要
Hypersonic flight vehicle faces critical challenges of control from highly nonlinear and time-varying uncertainties, which impose stringent requirements for real-time parameter adaptation under safety constraints. This paper proposes a reinforcement learning-based adaptive tracking control algorithm to address these issues. The crucial contributions of our design, as opposed to the state-of-the-art approaches, lie in three aspects: 1) a hybrid design of model-based control and reinforcement learning to alleviate the safety, stability and generalization issues of learning-based methods specifically for the demanding hypersonic flight environment; 2) the establishment of a reinforcement learning-based optimization framework that dynamically adjusts control parameters in a real-time optimal fashion to improve the tracking performance under dynamic uncertainties and flight regime transitions, which is substantially different from most conventional methods with constant parameters; 3) the theoretical analysis of both the closed-loop stability of the adaptive control and the convergence performance of the learning algorithm, which distinguishes our design from most existing reinforcement learning-based methods that have no stability or convergence guarantee and is particularly critical for safety-critical hypersonic flight vehicle applications. Numerical simulations show that the proposed method achieves a reduction in the integral of tracking error of 8.31% under model perturbations and 34.3% under changing reference trajectories, compared to the baseline method, while maintaining comparable control energy consumption.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 784-797 |
| 页数 | 14 |
| 期刊 | IEEE Transactions on Automation Science and Engineering |
| 卷 | 23 |
| DOI | |
| 出版状态 | 已出版 - 2026 |
联合国可持续发展目标
此成果有助于实现下列可持续发展目标:
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可持续发展目标 7 经济适用的清洁能源
学术指纹
探究 'Deep Reinforcement Learning-Driven Parameter Tuning for Adaptive Control Systems in Hypersonic Flight Vehicle' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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