Fuzzy-Adaptive Nonsingular Terminal Sliding Mode Control for the High-Speed Aircraft Actuator Trajectory Tracking

Fuzzy-Adaptive Nonsingular Terminal Sliding Mode Control for the High-Speed Aircraft Actuator Trajectory Tracking

High-speed aircraft actuators are critical for precise control of aerodynamic surfaces, demanding fast response, accuracy, and robustness against uncertainties and disturbances. However, the complex nonlinear dynamics of these systems pose significant challenges for conventional control methods. Sli...

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Bibliographic Details
Main Authors: Tieniu Chen, Xiaozhou He, Yunjiang Lou, Houde Liu, Lunfei Liang, Kunfeng Zhang
Format: Article
Language:English
Published: MDPI AG 2025-06-01
Series:Aerospace
Subjects:
high-speed aircraft actuator
nonlinear dynamics
sliding mode control
fuzzy logic
Online Access:https://www.mdpi.com/2226-4310/12/7/578
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