Composite Continuous High-Order Nonsingular Terminal Sliding Mode Control for Flying Wing UAVs with Disturbances and Actuator Faults

Flying wing UAVs are widely used in both civil and military areas and they are vulnerable to being affected by multi-source disturbances and actuator faults due to their unique aerodynamic configuration. This paper proposes composite continuous high-order nonsingular terminal sliding mode control co...

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Bibliographic Details

Published in:	Mathematics
Main Authors:	Hao Wang, Zhenhua Zhao
Format:	Article
Language:	English
Published:	MDPI AG 2025-07-01
Subjects:	terminal sliding mode control sliding mode observer flying wing UAVs finite-time control disturbance rejection control
Online Access:	https://www.mdpi.com/2227-7390/13/15/2375