控制理论(社会学)
计算机科学
姿态控制
非线性系统
李雅普诺夫函数
空气动力学
高超音速
趋同(经济学)
强化学习
理论(学习稳定性)
控制工程
控制(管理)
人工智能
工程类
物理
量子力学
机器学习
经济增长
经济
航空航天工程
作者
Zheng Wang,Tianyi Wu,Zhanxia Zhu,Chunhe Ma
出处
期刊:Journal of Aerospace Engineering
[American Society of Civil Engineers]
日期:2024-01-11
卷期号:37 (2)
被引量:2
标识
DOI:10.1061/jaeeez.aseng-5008
摘要
This paper proposes a reinforcement learning–based adaptive attitude control (RLAC) method for a class of hypersonic flight vehicles (HFVs) output constrained nonaffine attitude control problems subject to unmatched disturbances. First, by considering the strong coupling of HFVs attitude dynamics, the uncertainty of aerodynamic parameters and the complexity of the flight environment, a second-order multivariable nonaffine nonlinear control system is obtained. Then, by introducing specific nonlinear function and coordinate transformation techniques, the output constrained nonaffine control problem is transformed into a stabilization problem of several new variables. Moreover, dual actor-critic networks and their adaptive weight update laws are designed to cope with unknown unmatched and matched structural uncertainties. Meanwhile, two super-twisting disturbance observers integrated with dual actor-critic networks are designed to compensate unknown unmatched and matched external disturbances. With the help of the Lyapunov direct method, output constraint, convergence of the estimated weights, and stability of the system are proved. Finally, the validity as well as superiority of the proposed method are verified by numerical simulations.
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