An Optimized Pressure-Based Method for Thrust Vectoring Angle Estimation

This research developed a pressure-based thrust vectoring angle estimation method for fluidic thrust vectoring nozzles. This method can accurately estimate the real-time in-flight thrust vectoring angle using only wall pressure information on the inner surface of the nozzle. We proposed an algorithm...

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Bibliographic Details
Main Authors: Nanxing Shi, Yunsong Gu, Tingting Wu, Yuhang Zhou, Yi Wang, Shuai Deng
Format: Article
Language:English
Published: MDPI AG 2023-11-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/12/978