TY - JOUR
T1 - Neural network-based simplified optimised backstepping control for attitude tracking of a 2-DOF helicopter system
AU - Zhu, Jiahao
AU - Li, Yuanzhe
AU - Wen, Guoxing
AU - Lee, Sangmoon
AU - Veluvolu, Kalyana C.
N1 - Publisher Copyright:
© 2025 Informa UK Limited, trading as Taylor & Francis Group.
PY - 2025
Y1 - 2025
N2 - This article proposes an adaptive optimised control strategy for attitude tracking in a 2-degrees-of-freedom (2-DOF) helicopter system by applying optimised backstepping (OB) technique. In order to derive the optimised control, the neural network (NN) approximation is implemented to obtain the estimated solution of Hamilton–Jacobi–Bellman (HJB) equation, and the NN is trained to utilise a simplified Reinforcement learning (RL) algorithm in the identifier–critic–actor architecture, which obtaining the training laws from the negative gradient of a straightforward positive function, rather than utilising established optimal control methodologies. The system's closed-loop error signals are proven to be Semi-Global Uniformly Ultimately Bounded (SGUUB), and output follows the reference signal precisely, as verified through Lyapunov analysis. Comparative simulation results demonstrate the effectiveness of the proposed strategy in practical engineering fields, particularly in optimising control for real-world systems.
AB - This article proposes an adaptive optimised control strategy for attitude tracking in a 2-degrees-of-freedom (2-DOF) helicopter system by applying optimised backstepping (OB) technique. In order to derive the optimised control, the neural network (NN) approximation is implemented to obtain the estimated solution of Hamilton–Jacobi–Bellman (HJB) equation, and the NN is trained to utilise a simplified Reinforcement learning (RL) algorithm in the identifier–critic–actor architecture, which obtaining the training laws from the negative gradient of a straightforward positive function, rather than utilising established optimal control methodologies. The system's closed-loop error signals are proven to be Semi-Global Uniformly Ultimately Bounded (SGUUB), and output follows the reference signal precisely, as verified through Lyapunov analysis. Comparative simulation results demonstrate the effectiveness of the proposed strategy in practical engineering fields, particularly in optimising control for real-world systems.
KW - 2-degrees-of-freedom (2-DOF) helicopter system
KW - attitude tracking
KW - neural network (NN)
KW - Optimised control
KW - reinforcement learning (RL)
UR - https://www.scopus.com/pages/publications/105012433651
U2 - 10.1080/00207179.2025.2540542
DO - 10.1080/00207179.2025.2540542
M3 - Article
AN - SCOPUS:105012433651
SN - 0020-7179
JO - International Journal of Control
JF - International Journal of Control
ER -