SG10201605667PA - System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit - Google Patents

System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit

Info

Publication number
SG10201605667PA
SG10201605667PA SG10201605667PA SG10201605667PA SG10201605667PA SG 10201605667P A SG10201605667P A SG 10201605667PA SG 10201605667P A SG10201605667P A SG 10201605667PA SG 10201605667P A SG10201605667P A SG 10201605667PA SG 10201605667P A SG10201605667P A SG 10201605667PA
Authority
SG
Singapore
Prior art keywords
maneuvering
computer program
program product
propulsion unit
air vehicle
Prior art date
Application number
SG10201605667PA
Other languages
English (en)
Inventor
Guy Dekel
Lior Zivan
Yoav Efraty
Amit Wolff
Avner Volovick
Original Assignee
Israel Aerospace Ind 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 Israel Aerospace Ind Ltd filed Critical Israel Aerospace Ind Ltd
Publication of SG10201605667PA publication Critical patent/SG10201605667PA/en

Links

Classifications

    • 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
    • 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
    • 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
    • B64C29/0033—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 tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B64U50/14—Propulsion using external fans or propellers ducted or shrouded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/60—Take-off or landing of UAVs from a runway using their own power
    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/296—Rotors with variable spatial positions relative to the UAV body
    • B64U30/297—Tilting rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Traffic Control Systems (AREA)
  • Hydraulic Control Valves For Brake Systems (AREA)
SG10201605667PA 2012-01-12 2013-01-10 System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit SG10201605667PA (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IL217501A IL217501A (en) 2012-01-12 2012-01-12 A method and system for maneuvering aircraft

Publications (1)

Publication Number Publication Date
SG10201605667PA true SG10201605667PA (en) 2016-09-29

Family

ID=46467073

Family Applications (2)

Application Number Title Priority Date Filing Date
SG10201605667PA SG10201605667PA (en) 2012-01-12 2013-01-10 System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit
SG11201404023PA SG11201404023PA (en) 2012-01-12 2013-01-10 System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit

Family Applications After (1)

Application Number Title Priority Date Filing Date
SG11201404023PA SG11201404023PA (en) 2012-01-12 2013-01-10 System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit

Country Status (7)

Country Link
US (2) US9731818B2 (fr)
EP (1) EP2802952B1 (fr)
KR (2) KR101849934B1 (fr)
IL (1) IL217501A (fr)
IN (1) IN2014MN01616A (fr)
SG (2) SG10201605667PA (fr)
WO (1) WO2013105094A1 (fr)

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IL217501A (en) 2017-09-28
KR20180041250A (ko) 2018-04-23
WO2013105094A1 (fr) 2013-07-18
US20140339372A1 (en) 2014-11-20
SG11201404023PA (en) 2014-08-28
IL217501A0 (en) 2012-06-28
US10474167B2 (en) 2019-11-12
US20180002004A1 (en) 2018-01-04
IN2014MN01616A (fr) 2015-07-03
KR102022011B1 (ko) 2019-09-17
US9731818B2 (en) 2017-08-15
KR20140114875A (ko) 2014-09-29
EP2802952B1 (fr) 2019-10-09
KR101849934B1 (ko) 2018-04-18
EP2802952A1 (fr) 2014-11-19

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