IN2014MN01616A - - Google Patents
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- Publication number
- IN2014MN01616A IN2014MN01616A IN1616MUN2014A IN2014MN01616A IN 2014MN01616 A IN2014MN01616 A IN 2014MN01616A IN 1616MUN2014 A IN1616MUN2014 A IN 1616MUN2014A IN 2014MN01616 A IN2014MN01616 A IN 2014MN01616A
- Authority
- IN
- India
- Prior art keywords
- tiltable
- air vehicle
- vector direction
- thrust vector
- control
- Prior art date
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
- 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
- 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
- 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
- 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
-
- 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
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (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)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IL217501A IL217501A (en) | 2012-01-12 | 2012-01-12 | A method and system for maneuvering aircraft |
| PCT/IL2013/050029 WO2013105094A1 (en) | 2012-01-12 | 2013-01-10 | System, method and computer program product for maneuvering of an air vehicle with tiltable propulsion unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IN2014MN01616A true IN2014MN01616A (es) | 2015-07-03 |
Family
ID=46467073
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN1616MUN2014 IN2014MN01616A (es) | 2012-01-12 | 2013-01-10 |
Country Status (7)
| Country | Link |
|---|---|
| US (2) | US9731818B2 (es) |
| EP (1) | EP2802952B1 (es) |
| KR (2) | KR102022011B1 (es) |
| IL (1) | IL217501A (es) |
| IN (1) | IN2014MN01616A (es) |
| SG (2) | SG11201404023PA (es) |
| WO (1) | WO2013105094A1 (es) |
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| DE102012104783B4 (de) * | 2012-06-01 | 2019-12-24 | Quantum-Systems Gmbh | Fluggerät, bevorzugt UAV, Drohne und/oder UAS |
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-
2012
- 2012-01-12 IL IL217501A patent/IL217501A/en active IP Right Grant
-
2013
- 2013-01-10 KR KR1020187010214A patent/KR102022011B1/ko active IP Right Grant
- 2013-01-10 WO PCT/IL2013/050029 patent/WO2013105094A1/en active Application Filing
- 2013-01-10 SG SG11201404023PA patent/SG11201404023PA/en unknown
- 2013-01-10 KR KR1020147022569A patent/KR101849934B1/ko active IP Right Grant
- 2013-01-10 SG SG10201605667PA patent/SG10201605667PA/en unknown
- 2013-01-10 IN IN1616MUN2014 patent/IN2014MN01616A/en unknown
- 2013-01-10 EP EP13703644.8A patent/EP2802952B1/en active Active
- 2013-01-10 US US14/372,060 patent/US9731818B2/en active Active
-
2017
- 2017-08-11 US US15/675,547 patent/US10474167B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US9731818B2 (en) | 2017-08-15 |
| KR102022011B1 (ko) | 2019-09-17 |
| WO2013105094A1 (en) | 2013-07-18 |
| KR20140114875A (ko) | 2014-09-29 |
| EP2802952A1 (en) | 2014-11-19 |
| SG11201404023PA (en) | 2014-08-28 |
| EP2802952B1 (en) | 2019-10-09 |
| IL217501A0 (en) | 2012-06-28 |
| US20180002004A1 (en) | 2018-01-04 |
| US10474167B2 (en) | 2019-11-12 |
| KR101849934B1 (ko) | 2018-04-18 |
| US20140339372A1 (en) | 2014-11-20 |
| SG10201605667PA (en) | 2016-09-29 |
| KR20180041250A (ko) | 2018-04-23 |
| IL217501A (en) | 2017-09-28 |
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