Mathematical Modelling and Fluidic Thrust Vectoring Control of a Delta Wing UAV

Pitch control of an unmanned aerial vehicle (UAV) using fluidic thrust vectoring (FTV) is a relatively novel technique requiring no moving control surfaces, such as elevators. In this paper, the authors’ previous work on the characterization of a static co-flow FTV rig is further validated using the...

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Bibliographic Details
Main Authors: Ahsan Tanveer, Sarvat Mushtaq Ahmad
Format: Article
Language:English
Published: MDPI AG 2023-06-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/6/563