TY - JOUR
T1 - Direct Lift Control for Carrier-Based Aircraft With Predefined-Time Incremental Strategy
AU - Li, Yu
AU - Liu, Xiaoxiong
AU - Zhen, Ziyang
AU - Wen, Chih Yung
AU - Zheng, Yuanshi
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2025/10
Y1 - 2025/10
N2 - Aiming at the issue of disturbance affecting carrier landing, this article proposes an incremental nonlinear control-based direct lift control (DLC) technology with a predefined-time property to improve the landing accuracy of carrier-based aircraft. First, the mechanism and advantages of the DLC strategy for carrier landings are analyzed from an aerodynamic perspective. Then, a predefined-time-based incremental control approach is proposed and applied to design the automatic carrier landing system with DLC, which addresses the issue of uncertainty in the convergence time of the existing landing systems. Importantly, a disturbance observer with predefined-time stability and a noise rejection filter are proposed to eliminate radar measurement disturbances. By employing the Lyapunov method, it is demonstrated that the designed landing system can ensure the altitude tracking error converges to a small region within a user-defined time. Finally, real-time simulation results demonstrate the effectiveness of the developed landing system and its superiority compared to existing studies.
AB - Aiming at the issue of disturbance affecting carrier landing, this article proposes an incremental nonlinear control-based direct lift control (DLC) technology with a predefined-time property to improve the landing accuracy of carrier-based aircraft. First, the mechanism and advantages of the DLC strategy for carrier landings are analyzed from an aerodynamic perspective. Then, a predefined-time-based incremental control approach is proposed and applied to design the automatic carrier landing system with DLC, which addresses the issue of uncertainty in the convergence time of the existing landing systems. Importantly, a disturbance observer with predefined-time stability and a noise rejection filter are proposed to eliminate radar measurement disturbances. By employing the Lyapunov method, it is demonstrated that the designed landing system can ensure the altitude tracking error converges to a small region within a user-defined time. Finally, real-time simulation results demonstrate the effectiveness of the developed landing system and its superiority compared to existing studies.
KW - Automatic carrier landing system (ACLS)
KW - direct lift control (DLC)
KW - incremental control
KW - predefined-time control
KW - radar measurement disturbance
UR - https://www.scopus.com/pages/publications/105005211473
U2 - 10.1109/TAES.2025.3569244
DO - 10.1109/TAES.2025.3569244
M3 - 文章
AN - SCOPUS:105005211473
SN - 0018-9251
VL - 61
SP - 11528
EP - 11542
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 5
ER -