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...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-06-01
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Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/10/6/563 |