Simultaneous tailplane of small UAV and autopilot system design
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 30 July 2019
Issue publication date: 21 October 2019
Abstract
Purpose
The purpose of this paper is to rise the autonomous flight performance of the small unmanned aerial vehicle (UAV) using simultaneous tailplane of UAV and autopilot system design.
Design/methodology/approach
A small UAV is remanufactured in the UAV laboratory. Its tailplane can be changed before the flight. Autopilot parameters and some parameters of tailplane are instantaneously designed to maximize autonomous flight performance using a stochastic optimization method. Results found are applied for simulations.
Findings
Benefitting simultaneous tailplane of UAV and autopilot system design process, autonomous flight performance is maximized.
Research limitations/implications
Authorization of Directorate General of Civil Aviation in Turkey is required for UAV flights.
Practical implications
Simultaneous tailplane and autopilot system design process is so useful for refining UAV autonomous flight performance.
Social implications
Simultaneous tailplane and autopilot system design process fulfills confidence, high autonomous performance, and easy service demands of UAV users. By that way, UAV users will be able to use better UAVs.
Originality/value
Creating a novel technique to recover autonomous flight performance (e.g. less overshoot, less settling time and less rise time during trajectory tracking) of UAV and developing a novel procedure performing simultaneous tailplane of UAV and autopilot system design idea.
Keywords
Acknowledgements
This work was supported by the Research Fund of Erciyes University Scientific Research Projects (BAP) Coordination Unit under Project Number: FBA-2018-6712.
This work was also supported by the Research Fund of The Scientific and Technological Research Council of Turkey (TÜBİTAK) under Project Number: 114M856.
The author would like to also recognize Assoc. Prof. Dr Tugrul OKTAY, Assist. Prof. Dr Mehmet KONAR and PhD Candidate Alpertunga CEYLAN for their supports during UAV manufacturing and UAV flight testing.
Citation
Çoban, S. (2019), "Simultaneous tailplane of small UAV and autopilot system design", Aircraft Engineering and Aerospace Technology, Vol. 91 No. 10, pp. 1308-1313. https://doi.org/10.1108/AEAT-03-2019-0043
Publisher
:Emerald Publishing Limited
Copyright © 2019, Emerald Publishing Limited