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

Design and development of a tilt-wing UAV

Sayfa
733–741
Yayın Tarihi
2011-05-01
DOI
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⚡ TL;DR(1 Cümlede Hızlı Çıkarım)

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

📌 3 Maddede Bu Makale

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Amaç & Hipotez: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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Temel Bulgular & Veri:Real flight tests show that the aerial vehicle can successfully operate in VTOL mode.
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Sonuç & Katkı:Kalman filtering is employed to obtain accurate roll and pitch angle estimations.
🔬Tür:Araştırma Makalesi
📍Kapsam:Genişletilmiş Akademik Örneklem
⚙️Değişkenler:UAV · quad tilt-wing · VTOL

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.

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.

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Bu Makaleye Atıf Yap

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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