Turbojet Thrust Augmentation through a Variable Exhaust Nozzle with Active Disturbance Rejection Control

Turbojet Thrust Augmentation through a Variable Exhaust Nozzle with Active Disturbance Rejection Control

Turbojets require variable exhaust nozzles to fit high-demanding applications; however, few reports on nozzle control are available. The purpose of this paper is to investigate the possible advantages of an exhaust gas control through a variable exhaust nozzle. The control design method combines suc...

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Bibliographic Details
Main Authors: Francisco Villarreal-Valderrama, Patricia Zambrano-Robledo, Diana Hernandez-Alcantara, Luis Amezquita-Brooks
Format: Article
Language:English
Published: MDPI AG 2021-10-01
Series:Aerospace
Subjects:
aircraft propulsion
variable exhaust nozzle
active disturbance rejection control
propulsion systems
Online Access:https://www.mdpi.com/2226-4310/8/10/293

Internet

https://www.mdpi.com/2226-4310/8/10/293

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