Roll Control of Morphing Aircraft with Synthetic Jet Actuators at a High Angle of Attack

Flow separation and dynamic stall occurring at a high angle of attack will lead to difficulty in control and maneuverability for morphing aircraft. This study proposes a novel active flow control technology using a synthetic jet actuator for the roll motion of morphing aircraft. With the help of the...

Ausführliche Beschreibung

Bibliografische Detailangaben

Hauptverfasser:	Wencheng Li, Wenyun Wang, Xiaomao Huang, Shun Zhang, Chenyang Li
Format:	Artigo
Sprache:	Inglês
Veröffentlicht:	MDPI AG 2021-01-01
Schriftenreihe:	Applied Sciences
Schlagworte:	morphing aircraft synthetic jet actuator sliding mode control input saturation constraint
Online-Zugang:	https://www.mdpi.com/2076-3417/11/2/505
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