AU2003269439A1 - Flight control system for vtol aircraft - Google Patents

Flight control system for vtol aircraft

Info

Publication number
AU2003269439A1
AU2003269439A1 AU2003269439A AU2003269439A AU2003269439A1 AU 2003269439 A1 AU2003269439 A1 AU 2003269439A1 AU 2003269439 A AU2003269439 A AU 2003269439A AU 2003269439 A AU2003269439 A AU 2003269439A AU 2003269439 A1 AU2003269439 A1 AU 2003269439A1
Authority
AU
Australia
Prior art keywords
control system
flight control
vtol aircraft
vtol
aircraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU2003269439A
Inventor
Raphael Yoeli
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Urban Aeronautics Ltd
Original Assignee
Urban Aeronautics Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Urban Aeronautics Ltd filed Critical Urban Aeronautics Ltd
Publication of AU2003269439A1 publication Critical patent/AU2003269439A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
AU2003269439A 2002-10-01 2003-09-30 Flight control system for vtol aircraft Abandoned AU2003269439A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US41462802P 2002-10-01 2002-10-01
US60/414,628 2002-10-01
PCT/IL2003/000786 WO2004031876A1 (en) 2002-10-01 2003-09-30 Flight control system for vtol aircraft

Publications (1)

Publication Number Publication Date
AU2003269439A1 true AU2003269439A1 (en) 2004-04-23

Family

ID=32069743

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003269439A Abandoned AU2003269439A1 (en) 2002-10-01 2003-09-30 Flight control system for vtol aircraft

Country Status (2)

Country Link
AU (1) AU2003269439A1 (en)
WO (1) WO2004031876A1 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6464166B1 (en) 2001-05-29 2002-10-15 Romeo Yankee Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
AU2002309237A1 (en) 2001-06-04 2002-12-16 Romeo Yankee Ltd. Vehicles particularly useful as vtol vehicles
US7857253B2 (en) 2003-10-27 2010-12-28 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
EP1855942A2 (en) 2005-01-10 2007-11-21 Urban Aeronautics Ltd. Ducted fan vtol vehicles
US7946528B2 (en) 2005-04-15 2011-05-24 Urban Aeronautics, Ltd. Flight control system especially suited for VTOL vehicles
US7717368B2 (en) 2005-06-07 2010-05-18 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
WO2007099543A2 (en) 2006-03-01 2007-09-07 Urban Aeronautics Ltd. Ground effect vanes arrangement
WO2008065654A2 (en) 2006-11-27 2008-06-05 Urban Aeronautics Ltd. Wall effects on vtol vehicles
WO2008135973A2 (en) 2007-05-02 2008-11-13 Urban Aeronautics Ltd. Control flows and forces in vtol vehicles
WO2010026517A2 (en) 2008-09-02 2010-03-11 Urban Aeronautics Ltd. Vtol vehicle with coaxially tilted or tiltable rotors
CN106708071A (en) * 2015-11-17 2017-05-24 北京鸣鑫航空科技有限公司 Highly-integrated autonomous flight micro UAV flight control system
CN105549603B (en) * 2015-12-07 2018-08-28 北京航空航天大学 A kind of Intelligent road inspection control method of multi-rotor unmanned aerial vehicle
CN118484028B (en) * 2024-07-16 2024-09-13 中国空气动力研究与发展中心计算空气动力研究所 Control method for mechanical-elastic separation compatibility based on preset rudder deflection

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3665809A (en) * 1970-08-19 1972-05-30 Abex Corp Multiple channel redundant control system
US4649484A (en) * 1983-08-01 1987-03-10 The Boeing Company Avionic control system
US7017861B1 (en) * 2000-05-22 2006-03-28 Saab Ab Control system for actuators in an aircraft
US6431494B1 (en) * 2001-07-17 2002-08-13 Sikorsky Aircraft Corporation Flight control system for a hybrid aircraft in the roll axis

Also Published As

Publication number Publication date
WO2004031876A1 (en) 2004-04-15

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase