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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Bibliografische gegevens

Hoofdauteurs:	Hao Wang, Zhenhua Zhao
Formaat:	Artigo
Taal:	Inglês
Gepubliceerd in:	MDPI AG 2025-07-01
Reeks:	Mathematics
Onderwerpen:	terminal sliding mode control sliding mode observer flying wing UAVs finite-time control disturbance rejection control
Online toegang:	https://www.mdpi.com/2227-7390/13/15/2375
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