TY - GEN
T1 - Autonomous Aerial Refueling Formation Flight Control Based on Finite-time Control under Wind Field Disturbance
AU - Duan, You
AU - Qu, Yaohong
AU - Zhao, Wenbi
N1 - Publisher Copyright:
© 2021 Technical Committee on Control Theory, Chinese Association of Automation.
PY - 2021/7/26
Y1 - 2021/7/26
N2 - In order to solve the problem that the aerial refueling formation has low accuracy and is greatly affected by wind disturbance, this paper proposes a finite-time stable formation control method based on three-dimensional guidance. First, a high-accuracy formation control method is proposed, which can eliminate the forward, lateral and longitudinal directions errors by controlling the track angle. Secondly, a formation controller based on finite-time control to resist wind field interference is designed. Finally, it is verified that the fast terminal sliding surface converge in a finite time on the basis of Lyapunov's stability theory. The simulation results show that the formation method combining three-dimensional guidance law and fast terminal sliding mode control can not only ensure that the formation distance error is less than 0.5m, but also improve the robustness of the system to reach the desired state quickly.
AB - In order to solve the problem that the aerial refueling formation has low accuracy and is greatly affected by wind disturbance, this paper proposes a finite-time stable formation control method based on three-dimensional guidance. First, a high-accuracy formation control method is proposed, which can eliminate the forward, lateral and longitudinal directions errors by controlling the track angle. Secondly, a formation controller based on finite-time control to resist wind field interference is designed. Finally, it is verified that the fast terminal sliding surface converge in a finite time on the basis of Lyapunov's stability theory. The simulation results show that the formation method combining three-dimensional guidance law and fast terminal sliding mode control can not only ensure that the formation distance error is less than 0.5m, but also improve the robustness of the system to reach the desired state quickly.
KW - Aerial Autonomous Refueling
KW - Fast terminal sliding mode control
KW - finite-time stability
KW - formation flight
UR - http://www.scopus.com/inward/record.url?scp=85117355322&partnerID=8YFLogxK
U2 - 10.23919/CCC52363.2021.9549643
DO - 10.23919/CCC52363.2021.9549643
M3 - 会议稿件
AN - SCOPUS:85117355322
T3 - Chinese Control Conference, CCC
SP - 7880
EP - 7885
BT - Proceedings of the 40th Chinese Control Conference, CCC 2021
A2 - Peng, Chen
A2 - Sun, Jian
PB - IEEE Computer Society
T2 - 40th Chinese Control Conference, CCC 2021
Y2 - 26 July 2021 through 28 July 2021
ER -