Sided performance coaxial vertical takeoff and landing (vtol) uav and pitch stability technique using oblique active tilting (oat)

Hamzeh Mahmoud Abde Quader Alzu'bi; Imad Abd Allateef; Yahya Zweiri; Basim Alkhateeb; Yahya Taha Ayed Al-Majali

Sided performance coaxial vertical takeoff and landing (vtol) uav and pitch stability technique using oblique active tilting (oat)

Hamzeh Mahmoud Abde Quader Alzu'bi (Inventor), Imad Abd Allateef (Inventor), Yahya Zweiri (Inventor), Basim Alkhateeb (Inventor), Yahya Taha Ayed Al-Majali (Inventor)

Research output: Patent

Original language	English
Patent number	US20130105620
Publication status	Published - May 2013

Bibliographical note

Patent applicant: King Abdullah II Design and Development Bureau

Keywords

Mechanical, aeronautical and manufacturing engineering

Access to Document

http://appft1.uspto.gov/netacgi/nph-Parser?Sect1=PTO1&Sect2=HITOFF&d=PG01&p=1&u=/netahtml/PTO/srchnum.html&r=1&f=G&l=50&s1=20130105620.PGNR.

Cite this

Abde Quader Alzu'bi, H. M., Abd Allateef, I., Zweiri, Y., Alkhateeb, B., & Al-Majali, Y. T. A. (2013). Sided performance coaxial vertical takeoff and landing (vtol) uav and pitch stability technique using oblique active tilting (oat). (Patent No. US20130105620). http://appft1.uspto.gov/netacgi/nph-Parser?Sect1=PTO1&Sect2=HITOFF&d=PG01&p=1&u=/netahtml/PTO/srchnum.html&r=1&f=G&l=50&s1=20130105620.PGNR.

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Abde Quader Alzu'bi, HM, Abd Allateef, I, Zweiri, Y, Alkhateeb, B & Al-Majali, YTA, Sided performance coaxial vertical takeoff and landing (vtol) uav and pitch stability technique using oblique active tilting (oat), Patent No. US20130105620. <http://appft1.uspto.gov/netacgi/nph-Parser?Sect1=PTO1&Sect2=HITOFF&d=PG01&p=1&u=/netahtml/PTO/srchnum.html&r=1&f=G&l=50&s1=20130105620.PGNR.>

TY - PAT

T1 - Sided performance coaxial vertical takeoff and landing (vtol) uav and pitch stability technique using oblique active tilting (oat)

AU - Abde Quader Alzu'bi, Hamzeh Mahmoud

AU - Abd Allateef, Imad

AU - Zweiri, Yahya

AU - Alkhateeb, Basim

AU - Al-Majali, Yahya Taha Ayed

N1 - Patent applicant: King Abdullah II Design and Development Bureau

PY - 2013/5

Y1 - 2013/5

KW - Mechanical, aeronautical and manufacturing engineering

M3 - Patent

M1 - US20130105620

ER -