Thrust Vectoring Control of a Novel Tilt-Rotor UAV Based on Backstepping Sliding Model Method

In this paper, a control method of a novel tilt-rotor UAV with a blended wing body layout is studied. The novel UAV is capable of vertical take-off and landing and has strong stealth capabilities that can be applied to carrier-borne reconnaissance aircraft. However, the high aspect ratio of blended...

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Bibliografske podrobnosti
Main Authors: Zelong Yu, Jingjuan Zhang, Xueyun Wang
Format: Article
Jezik:English
Izdano: MDPI AG 2023-01-01
Serija:Sensors
Teme:
Online dostop:https://www.mdpi.com/1424-8220/23/2/574

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