TY - JOUR
T1 - Reinforcement Learning-Based Integrated Decision-Making and Control for Morphing Flight Vehicles Under Aerodynamic Uncertainties
AU - Guo, Zongyi
AU - Cao, Shiyuan
AU - Yuan, Ruizhe
AU - Guo, Jianguo
AU - Zhang, Yuan
AU - Li, Jingyuan
AU - Hu, Guanjie
AU - Han, Yonglin
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2024
Y1 - 2024
N2 - This article presents an integrated decision-making and control framework of morphing flight vehicles with variable-span wings in the glide phase. The proposed framework comprehensively consists of morphing strategy, attitude control, and online aerodynamic uncertainties estimate, thus outperforms existing works at its capacity of adequately considering the interaction between morphing mechanism and control design. Furthermore, the introduction of deep deterministic policy gradient algorithm has the effect of reducing the dependence on a precise model to some extent. By introducing aerodynamic uncertainties into the training environment and employing estimate, the framework enhances decision-making adaptability. In addition, the decision-making method is designed to optimal a comprehensive performance index including lift-to-drag ratio and attitude tracking effect, thus ensuring the physical realizability. The effectiveness of decision-making and control is validated by simulation results.
AB - This article presents an integrated decision-making and control framework of morphing flight vehicles with variable-span wings in the glide phase. The proposed framework comprehensively consists of morphing strategy, attitude control, and online aerodynamic uncertainties estimate, thus outperforms existing works at its capacity of adequately considering the interaction between morphing mechanism and control design. Furthermore, the introduction of deep deterministic policy gradient algorithm has the effect of reducing the dependence on a precise model to some extent. By introducing aerodynamic uncertainties into the training environment and employing estimate, the framework enhances decision-making adaptability. In addition, the decision-making method is designed to optimal a comprehensive performance index including lift-to-drag ratio and attitude tracking effect, thus ensuring the physical realizability. The effectiveness of decision-making and control is validated by simulation results.
KW - Attitude control
KW - decision-making
KW - extended Kalman filter (EKF)
KW - morphing flight vehicles (MFVs)
KW - reinforcement learning
UR - http://www.scopus.com/inward/record.url?scp=85200801075&partnerID=8YFLogxK
U2 - 10.1109/TAES.2024.3440969
DO - 10.1109/TAES.2024.3440969
M3 - 文章
AN - SCOPUS:85200801075
SN - 0018-9251
VL - 60
SP - 9342
EP - 9353
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 6
ER -