Design and initial flight tests of a holonomic quadrotor UAV with sub-rotor control surfaces
Küçük Resim Yok
Tarih
2013
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Erişim Hakkı
info:eu-repo/semantics/closedAccess
Özet
In this work, design and flight test prototype of a quadrotor helicopter UAV with sub-rotor control surfaces for non-inclined horizontal motion are described. Initial flight test results acquired from the prototype of the proposed UAV are presented in order to reveal the functionality of the new approach.
Açıklama
20th Annual International Conference on Mechatronics and Machine Vision in Practice, M2VIP 2013 -- 20 September 2013 through 20 September 2013 -- Ankara -- 102276
Anahtar Kelimeler
Design, Flight test, Holonomic, Quadrotor, Tilting wing, UAV
Kaynak
20th Annual International Conference on Mechatronics and Machine Vision in Practice, M2VIP 2013
WoS Q Değeri
Scopus Q Değeri
N/A
