Hybrid propulsion system design of a VTOL tailsitter UAV

Mirac Aksugur; Gokhan Inalhan; Randy Beard

doi:10.4271/2008-01-2242

Hybrid propulsion system design of a VTOL tailsitter UAV

Mirac Aksugur^*
, Gokhan Inalhan
, Randy Beard

^*Bu çalışma için yazışmadan sorumlu yazar

Uçak Mühendisliği Bölümü

Araştırma sonucu: Dergiye katkı › Konferans makalesi › bilirkişi

Özet

Tailsitter UAVs with their combined vertical take off and landing (VTOL) and fixed-wing aircraft with full flight-speed regime capability provides a distinct alternative to rotary-wing and ducted fan UAVs (OAVs). ITU-BYU Tailsitter concept aims to obtain the energy efficient regimes across the VTOL and the cruising flight regimes. This paper describes the hybrid propulsion system design approach to attain this. The preliminary design and the analysis indicate advantageous performance over other mini-class unmanned air vehicles.

Orijinal dil	İngilizce
Dergi	SAE Technical Papers
DOI'lar	https://doi.org/10.4271/2008-01-2242
Yayın durumu	Yayınlandı - 2008
Etkinlik	Wichita Aviation Technology Congress and Exhibition - Wichita, KS, United States Süre: 19 Ağu 2008 → 21 Ağu 2008

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10.4271/2008-01-2242

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Link to publication in Scopus

Alıntı Yap

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title = "Hybrid propulsion system design of a VTOL tailsitter UAV",

abstract = "Tailsitter UAVs with their combined vertical take off and landing (VTOL) and fixed-wing aircraft with full flight-speed regime capability provides a distinct alternative to rotary-wing and ducted fan UAVs (OAVs). ITU-BYU Tailsitter concept aims to obtain the energy efficient regimes across the VTOL and the cruising flight regimes. This paper describes the hybrid propulsion system design approach to attain this. The preliminary design and the analysis indicate advantageous performance over other mini-class unmanned air vehicles.",

author = "Mirac Aksugur and Gokhan Inalhan and Randy Beard",

year = "2008",

doi = "10.4271/2008-01-2242",

language = "English",

journal = "SAE Technical Papers",

issn = "0148-7191",

publisher = "SAE International",

note = "Wichita Aviation Technology Congress and Exhibition ; Conference date: 19-08-2008 Through 21-08-2008",

}

TY - JOUR

T1 - Hybrid propulsion system design of a VTOL tailsitter UAV

AU - Aksugur, Mirac

AU - Inalhan, Gokhan

AU - Beard, Randy

PY - 2008

Y1 - 2008

N2 - Tailsitter UAVs with their combined vertical take off and landing (VTOL) and fixed-wing aircraft with full flight-speed regime capability provides a distinct alternative to rotary-wing and ducted fan UAVs (OAVs). ITU-BYU Tailsitter concept aims to obtain the energy efficient regimes across the VTOL and the cruising flight regimes. This paper describes the hybrid propulsion system design approach to attain this. The preliminary design and the analysis indicate advantageous performance over other mini-class unmanned air vehicles.

AB - Tailsitter UAVs with their combined vertical take off and landing (VTOL) and fixed-wing aircraft with full flight-speed regime capability provides a distinct alternative to rotary-wing and ducted fan UAVs (OAVs). ITU-BYU Tailsitter concept aims to obtain the energy efficient regimes across the VTOL and the cruising flight regimes. This paper describes the hybrid propulsion system design approach to attain this. The preliminary design and the analysis indicate advantageous performance over other mini-class unmanned air vehicles.

UR - https://www.scopus.com/pages/publications/85072482599

U2 - 10.4271/2008-01-2242

DO - 10.4271/2008-01-2242

M3 - Conference article

AN - SCOPUS:85072482599

SN - 0148-7191

JO - SAE Technical Papers

JF - SAE Technical Papers

T2 - Wichita Aviation Technology Congress and Exhibition

Y2 - 19 August 2008 through 21 August 2008

ER -

Hybrid propulsion system design of a VTOL tailsitter UAV

Özet

BM SKH

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