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

^*Corresponding author for this work

Department of Aeronautical Engineering

Istanbul Technical University
Brigham Young University

Research output: Contribution to journal › Conference article › peer-review

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.

Original language	English
Journal	SAE Technical Papers
DOIs	https://doi.org/10.4271/2008-01-2242
Publication status	Published - 2008
Event	Wichita Aviation Technology Congress and Exhibition - Wichita, KS, United States Duration: 19 Aug 2008 → 21 Aug 2008

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Access to Document

10.4271/2008-01-2242

Cite this

@article{3872ad2f75294a81900faa4a992fa158,

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

Abstract

UN SDGs

Access to Document

Other files and links

Fingerprint

Cite this