Design and modeling of a gas-electric hybrid quad tilt-rotor UAV with morphing wing
Küçük Resim Yok
Tarih
2014
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
IEEE Computer Society
Erişim Hakkı
info:eu-repo/semantics/closedAccess
Özet
In this work, a gas-electric hybrid quad tilt-rotor UAV with morphing wing is designed. The mechanical design, propulsion system design and control architecture are explained. Dynamic model of the aerial vehicle is developed including the effects of tilting rotors, variable fuel weight, and morphing wing lift-drag forces and pitching moments. © 2014 IEEE.
Açıklama
11th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2014 -- 3 August 2014 through 6 August 2014 -- Tianjin -- 107410
Anahtar Kelimeler
gas-electric hybrid, morphing wing, Quad tilt-rotor UAV
Kaynak
2014 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2014
WoS Q Değeri
N/A
Scopus Q Değeri
N/A
