Journals / Turkish Journal of Electrical Engineering and Computer Science / 2011 / Cilt: 19 - Sayı: 5

Design and development of a tilt-wing UAV

Pages
733–741
Publication Date
2011-05-01
DOI
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

Kalman filtering is employed to obtain accurate roll and pitch angle estimations.

📌 3 Key Takeaways

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Objective & Hypothesis:In this paper, the mechanical and aerodynamic design, carbon composite production, hierarchical control system design and vertical flight tests of a new unmanned aerial vehicle (UAV), which is capable of VTOL (vertical takeoff and landing) like a helicopter and long range horizontal flight like an airplane, are presented.
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Key Findings & Data:Real flight tests show that the aerial vehicle can successfully operate in VTOL mode.
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Conclusion & Impact:Kalman filtering is employed to obtain accurate roll and pitch angle estimations.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:UAV · quad tilt-wing · VTOL

Abstract

In this paper, the mechanical and aerodynamic design, carbon composite production, hierarchical control system design and vertical flight tests of a new unmanned aerial vehicle (UAV), which is capable of VTOL (vertical takeoff and landing) like a helicopter and long range horizontal flight like an airplane, are presented. Real flight tests show that the aerial vehicle can successfully operate in VTOL mode. Kalman filtering is employed to obtain accurate roll and pitch angle estimations.

Özet

In this paper, the mechanical and aerodynamic design, carbon composite production, hierarchical control system design and vertical flight tests of a new unmanned aerial vehicle (UAV), which is capable of VTOL (vertical takeoff and landing) like a helicopter and long range horizontal flight like an airplane, are presented. Real flight tests show that the aerial vehicle can successfully operate in VTOL mode. Kalman filtering is employed to obtain accurate roll and pitch angle estimations.

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Cite This Article

ÇETİNSOY, E., SIRIMOĞLU, E., ÖNER, K. T., HANÇER, C., ÜNEL, M., AKŞİT, M. F., KANDEMİR, İ., GÜLEZ, K. (2011). Design and development of a tilt-wing UAV. Turkish Journal of Electrical Engineering and Computer Science, Cilt: 19 - Sayı: 5, 733–741. https://ajindex.com/articles/188695

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