Design of a Quad-Jet VTOL UAS for Heavy-lift Applications

Abdullah Turkmen; Erdinc Altug

doi:10.1109/ICUAS48674.2020.9214047

Design of a Quad-Jet VTOL UAS for Heavy-lift Applications

Abdullah Turkmen, Erdinc Altug

Makina Mühendisliği Bölümü

Istanbul Technical University

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

6 Atıf (Scopus)

Özet

Payload capacity, range and flight duration of a Unmanned Aerial System (UAS) depends mainly on thrust system. Thrust system of a typical electrical multi-rotor UAS consists of electric motors, rotors and electric speed controllers (ESCs). Electric motors are easy to use and their response time is short, which is highly desired and required for control, but they limit potential payload capacity, range and flight duration. In this paper, we propose a Quad-Jet VTOL (vertical take-off and land) UAS with a thrust system consisting of four mini jet engines. Such a vehicle could be useful heavy-lift applications. The UAS model, controllers, thrust direction system (to overcome the response time disadvantage and to improve motion) are presented, along with a first prototype system.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	875-882
Sayfa sayısı	8
ISBN (Elektronik)	9781728142777
DOI'lar	https://doi.org/10.1109/ICUAS48674.2020.9214047
Yayın durumu	Yayınlandı - Eyl 2020
Etkinlik	2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020 - Athens, Greece Süre: 1 Eyl 2020 → 4 Eyl 2020

Yayın serisi

Adı	2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???	2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
Ülke/Bölge	Greece
Şehir	Athens
Periyot	1/09/20 → 4/09/20

Bibliyografik not

Publisher Copyright:
© 2020 IEEE.

Finansman

ACKNOWLEDGEMENTS We would like to thank The Scientific and Technological Research Council of Turkey (TUBITAK) for funding project 118E192. We would also like to thank Mr. Yusuf Korkut and Mr. M. Okan Güney for their generous help in building the prototype.

Finansörler	Finansör numarası
TUBITAK	118E192
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu

BM SKH

Bu sonuç, aşağıdaki Sürdürülebilir Kalkınma Hedefine/Hedeflerine katkıda bulunur

Belgeye Erişim

10.1109/ICUAS48674.2020.9214047

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Turkmen, A., & Altug, E. (2020). Design of a Quad-Jet VTOL UAS for Heavy-lift Applications. In 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020 (pp. 875-882). Makale 9214047 (2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICUAS48674.2020.9214047

@inproceedings{2bf7835873a04e85b5814c249e427214,

title = "Design of a Quad-Jet VTOL UAS for Heavy-lift Applications",

abstract = "Payload capacity, range and flight duration of a Unmanned Aerial System (UAS) depends mainly on thrust system. Thrust system of a typical electrical multi-rotor UAS consists of electric motors, rotors and electric speed controllers (ESCs). Electric motors are easy to use and their response time is short, which is highly desired and required for control, but they limit potential payload capacity, range and flight duration. In this paper, we propose a Quad-Jet VTOL (vertical take-off and land) UAS with a thrust system consisting of four mini jet engines. Such a vehicle could be useful heavy-lift applications. The UAS model, controllers, thrust direction system (to overcome the response time disadvantage and to improve motion) are presented, along with a first prototype system.",

author = "Abdullah Turkmen and Erdinc Altug",

note = "Publisher Copyright: {\textcopyright} 2020 IEEE.; 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020 ; Conference date: 01-09-2020 Through 04-09-2020",

year = "2020",

month = sep,

doi = "10.1109/ICUAS48674.2020.9214047",

language = "English",

series = "2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "875--882",

booktitle = "2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020",

address = "United States",

}

Turkmen, A & Altug, E 2020, Design of a Quad-Jet VTOL UAS for Heavy-lift Applications. in 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020., 9214047, 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020, Institute of Electrical and Electronics Engineers Inc., pp. 875-882, 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020, Athens, Greece, 1/09/20. https://doi.org/10.1109/ICUAS48674.2020.9214047

Design of a Quad-Jet VTOL UAS for Heavy-lift Applications. / Turkmen, Abdullah; Altug, Erdinc.
2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020. Institute of Electrical and Electronics Engineers Inc., 2020. p. 875-882 9214047 (2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020).

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

TY - GEN

T1 - Design of a Quad-Jet VTOL UAS for Heavy-lift Applications

AU - Turkmen, Abdullah

AU - Altug, Erdinc

PY - 2020/9

Y1 - 2020/9

N2 - Payload capacity, range and flight duration of a Unmanned Aerial System (UAS) depends mainly on thrust system. Thrust system of a typical electrical multi-rotor UAS consists of electric motors, rotors and electric speed controllers (ESCs). Electric motors are easy to use and their response time is short, which is highly desired and required for control, but they limit potential payload capacity, range and flight duration. In this paper, we propose a Quad-Jet VTOL (vertical take-off and land) UAS with a thrust system consisting of four mini jet engines. Such a vehicle could be useful heavy-lift applications. The UAS model, controllers, thrust direction system (to overcome the response time disadvantage and to improve motion) are presented, along with a first prototype system.

AB - Payload capacity, range and flight duration of a Unmanned Aerial System (UAS) depends mainly on thrust system. Thrust system of a typical electrical multi-rotor UAS consists of electric motors, rotors and electric speed controllers (ESCs). Electric motors are easy to use and their response time is short, which is highly desired and required for control, but they limit potential payload capacity, range and flight duration. In this paper, we propose a Quad-Jet VTOL (vertical take-off and land) UAS with a thrust system consisting of four mini jet engines. Such a vehicle could be useful heavy-lift applications. The UAS model, controllers, thrust direction system (to overcome the response time disadvantage and to improve motion) are presented, along with a first prototype system.

UR - http://www.scopus.com/inward/record.url?scp=85094976456&partnerID=8YFLogxK

U2 - 10.1109/ICUAS48674.2020.9214047

DO - 10.1109/ICUAS48674.2020.9214047

M3 - Conference contribution

AN - SCOPUS:85094976456

T3 - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020

SP - 875

EP - 882

BT - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020

Y2 - 1 September 2020 through 4 September 2020

ER -

Design of a Quad-Jet VTOL UAS for Heavy-lift Applications

Özet

Yayın serisi

???event.eventtypes.event.conference???

Bibliyografik not

Finansman

BM SKH

Belgeye Erişim

Diğer Dosyalar ve Linkler

Parmak izi

Alıntı Yap