Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Cevdet Hançer"'
Publikováno v:
Journal of Aerospace Engineering. 25:574-587
This paper presents aerodynamic design and characterization of a new quad tilt-wing unmanned aerial vehicle [Sabanci University unmanned aerial vehicle (SUAVI)] through wind tunnel tests and provides experimental data for the design of similar aerial
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8aa3bd6f8956c705af4d48506eefea52
https://doi.org/10.1061/(asce)as.1943-5525.0000161
https://doi.org/10.1061/(asce)as.1943-5525.0000161
Autor:
Mustafa Unel, Cevdet Hançer, Serhat Dikyar, Mahmut Faruk Aksit, Ertuğrul Çetinsoy, Efe Sırımoğlu, Kaan Taha Öner
Publikováno v:
Mechatronics. 22:723-745
This paper presents aerodynamic and mechanical design, prototyping and flight control system design of a new unmanned aerial vehicle SUAVI ( S abanci University U nmanned A erial V eh I cle). SUAVI is an electric powered quad tilt-wing UAV that is ca
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e778bb17ad808a45ad3b6f71029c5368
https://doi.org/10.1016/j.mechatronics.2012.03.003
https://doi.org/10.1016/j.mechatronics.2012.03.003
Autor:
Ertuğrul Çetinsoy, Mustafa Unel, Efe Sırımoğlu, Kayhan Gulez, Cevdet Hançer, İlyas Kandemir, Mahmut Faruk Aksit, Kaan Taha Öner
Publikováno v:
Volume: 19, Issue: 5 733-741
Turkish Journal of Electrical Engineering and Computer Science
Turkish Journal of Electrical Engineering and Computer Science
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 hel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a85a7d497a61c47d5d12c91c9a294d2b
https://dergipark.org.tr/tr/pub/tbtkelektrik/issue/12067/144280
https://dergipark.org.tr/tr/pub/tbtkelektrik/issue/12067/144280
Autor:
Cevdet Hançer, Mustafa Unel, Kayhan Gulez, Mahmut Faruk Aksit, Ertuğrul Çetinsoy, Efe Sirimoğlu, Kaan Taha Öner, İlyas Kandemir
Publikováno v:
Volume: 20, Issue: 1 149-157
Turkish Journal of Electrical Engineering and Computer Science
Turkish Journal of Electrical Engineering and Computer Science
This paper presents a mathematical model and vertical flight control algorithms for a new tilt-wing unmanned aerial vehicle (UAV). The vehicle is capable of vertical take-off and landing (VTOL). Due to its tilt-wing structure, it can also fly horizon
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::daa7e639b69c5f28d23b8d67b7a7f5d5
https://doi.org/10.3906/elk-1007-624
https://doi.org/10.3906/elk-1007-624
Publikováno v:
CDC
This paper presents a robust position controller for a tilt-wing quadrotor to track desired trajectories under external wind and aerodynamic disturbances. Wind effects are modeled using Dryden model and are included in the dynamic model of the vehicl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::066a97afc6daa8cbfb10051813616f8c
https://doi.org/10.1109/cdc.2010.5717283
https://doi.org/10.1109/cdc.2010.5717283
Publikováno v:
IECON 2010 - 36th Annual Conference on IEEE Industrial Electronics Society.
This paper presents design of a robust hovering controller for a quad tilt-wing UAV to hover at a desired position under external wind and aerodynamic disturbances. Wind and the aerodynamic disturbances are modeled using the Dryden model. In order to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ba9ccdf607791d048060e5bff73c41b6
https://doi.org/10.1109/iecon.2010.5675441
https://doi.org/10.1109/iecon.2010.5675441