Improved Thrust Performance Optimization Method for UAVs Based on the Adaptive Margin Control Approach

This study proposes a strategy for improving the thrust performance of fixed-wing UAV turbine engines from the perspective of aircraft/engine integration. In the UAV engine control process, the inlet distortion caused by the angle of attack change is taken into account, the inlet distortion index is...

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Bibliographic Details

Published in:	Mathematics
Main Authors:	Yeguang Wang, Honglin Liu, Kai Liu
Format:	Article
Language:	English
Published:	MDPI AG 2023-02-01
Subjects:	unmanned aerial vehicle aircraft/engine integration thrust optimization adaptive margin model adaptive disturbance rejection control
Online Access:	https://www.mdpi.com/2227-7390/11/5/1176