TY - JOUR
T1 - Explainable deep reinforcement learning for three-axis robust attitude control of flying wing aircraft
AU - Yue, Ting
AU - Huo, Chunlin
AU - Wang, Lixin
AU - Liu, Hailiang
AU - Hu, Yanguo
AU - Tai, Shang
N1 - Publisher Copyright:
© 2026 Elsevier Masson SAS.
PY - 2026/11
Y1 - 2026/11
N2 - Owing to the absence of horizontal and vertical tails and the reliance on drag rudders for yaw control, flying wing aircraft exhibit distinct aerodynamic coupling and three-axis motion-coupling characteristics. Consequently, the flight control law design method must simultaneously address external turbulence, model parameter uncertainty, and strong coupling. In this paper, a neural network (NN)-based robust three-axis attitude control method utilizing the proximal policy optimization (PPO) algorithm is proposed. First, the state space of the agent is augmented by incorporating coupling states to eliminate the three-axis coupling and time-lagged states, which compensates for the servo-actuator delay. Second, a hierarchical-reward shaping strategy comprising subgoals for tracking accuracy, stability, and actuator-rate limits induces a piecewise control mechanism, thereby increasing robustness. Third, a progressive three-axis assisted training scheme is introduced to sequentially train the longitudinal, lateral, and directional networks and ensure accurate tracking and effective decoupling. Finally, kernel SHapley Additive exPlanations (Kernel SHAP) is employed to visualize the attributions of the state features. The time histories of the Shapley attribution, interpreted within the flight dynamics framework, elucidate the control mechanism, the compensation mechanism, and the sources of robustness for the NN controllers. The simulation results indicate that the proposed NN controllers achieve rapid and highly precise command tracking while maintaining stable and robust performance, even under severe atmospheric turbulence and significant model parameter perturbations.
AB - Owing to the absence of horizontal and vertical tails and the reliance on drag rudders for yaw control, flying wing aircraft exhibit distinct aerodynamic coupling and three-axis motion-coupling characteristics. Consequently, the flight control law design method must simultaneously address external turbulence, model parameter uncertainty, and strong coupling. In this paper, a neural network (NN)-based robust three-axis attitude control method utilizing the proximal policy optimization (PPO) algorithm is proposed. First, the state space of the agent is augmented by incorporating coupling states to eliminate the three-axis coupling and time-lagged states, which compensates for the servo-actuator delay. Second, a hierarchical-reward shaping strategy comprising subgoals for tracking accuracy, stability, and actuator-rate limits induces a piecewise control mechanism, thereby increasing robustness. Third, a progressive three-axis assisted training scheme is introduced to sequentially train the longitudinal, lateral, and directional networks and ensure accurate tracking and effective decoupling. Finally, kernel SHapley Additive exPlanations (Kernel SHAP) is employed to visualize the attributions of the state features. The time histories of the Shapley attribution, interpreted within the flight dynamics framework, elucidate the control mechanism, the compensation mechanism, and the sources of robustness for the NN controllers. The simulation results indicate that the proposed NN controllers achieve rapid and highly precise command tracking while maintaining stable and robust performance, even under severe atmospheric turbulence and significant model parameter perturbations.
KW - Explainable deep reinforcement learning
KW - Flying wing aircraft
KW - Neural network controller
KW - Robust control
KW - Shapley additive explanations
UR - https://www.scopus.com/pages/publications/105037434139
U2 - 10.1016/j.ast.2026.112472
DO - 10.1016/j.ast.2026.112472
M3 - 文章
AN - SCOPUS:105037434139
SN - 1270-9638
VL - 178
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 112472
ER -