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Control System Design of a Vertical Take-off and Landing Fixed-Wing UAV
Date
2016-05-20
Author
Cakici, Ferit
Leblebicioğlu, Mehmet Kemal
Metadata
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This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
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In this study, design and implementation of control system of a vertical take-off and landing (VTOL) unmanned aerial vechicle (UAV) with level flight capability is considered. The platform structure includes both multirotor and fixed-wing (FW) conventional aircraft control surfaces: therefore named as VTOL-FW. The proposed method includes implementation of multirotor and airplane controllers and design of an algorithm to switch between them in achieving transitions between VTOL and FW flight modes. Thus, VTOL-FW UAV's flight characteristics are expected to be improved by enabling agile maneuvers, increasing survivability and exploiting full flight envelope capabilities. (C) 2016, IFAC (International Federation of Antomatic Control) Hosting by Elsevier Ltd. All rights reserved.
Subject Keywords
Aircraft control
,
Autopilot
,
Mathematical modelling
,
Control. PID control
,
VTOL
,
UAV
URI
https://hdl.handle.net/11511/42976
DOI
https://doi.org/10.1016/j.ifacol.2016.07.045
Collections
Department of Electrical and Electronics Engineering, Conference / Seminar