Data-Driven Tracking Control for Nonaffine Yaw Channel of Helicopter via Off-Policy Reinforcement Learning

被引:11
作者
Zhang, Kun [1 ]
Luo, Shijie [1 ]
Wu, Huai-Ning [2 ,3 ]
Su, Rong [3 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China
[3] Nanyang Technol Univ, Sch Elect & Elect Engn, Singapore 311115, Singapore
基金
中国国家自然科学基金;
关键词
Heuristic algorithms; Aerodynamics; Rotors; Vehicle dynamics; Nonlinear dynamical systems; Tail; Stability criteria; Reinforcement learning; Mathematical models; Games; Adaptive dynamic programming (ADP); nonaffine systems; reinforcement learning (RL); tracking control; uncrewed aerial vehicle (UAV) helicopter; CONTINUOUS-TIME SYSTEMS;
D O I
10.1109/TAES.2025.3539264
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article presents an off-policy tracking control scheme for the continuous-time nonaffine yaw channel of uncrewed aerial vehicle helicopter. First, the article constructs an affine augmented system (AAS) within a parallel control structure to convert the original nonaffine tracking error dynamics into affine dynamics. Second, the article derives a stability criterion linking the nonaffine system and the AAS, demonstrating that the obtained zero-sum policy from the AAS can achieve the $H_\infty$ performance of the nonaffine system. Third, a data-driven off-policy tracking algorithm is designed for approximating the zero-sum solution of the Hamilton-Jacobi-Isaacs equations with unknown dynamics. Moreover, the recursive least squares process with a variable forgetting factor is employed to update the actor-critic neural network weights, with the algorithm's convergence being proven. Then, the uniformly ultimately bounded of tracking errors is guaranteed. Finally, two application examples are offered in simulation to validate the effectiveness of this presented method.
引用
收藏
页码:7725 / 7737
页数:13
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