ES2603430A1 - Sistema de detección y procedimiento de contacto de punta del botalón volador y boca del receptáculo para operaciones de repostaje aéreo con botalón - Google Patents
Sistema de detección y procedimiento de contacto de punta del botalón volador y boca del receptáculo para operaciones de repostaje aéreo con botalón Download PDFInfo
- Publication number
- ES2603430A1 ES2603430A1 ES201630480A ES201630480A ES2603430A1 ES 2603430 A1 ES2603430 A1 ES 2603430A1 ES 201630480 A ES201630480 A ES 201630480A ES 201630480 A ES201630480 A ES 201630480A ES 2603430 A1 ES2603430 A1 ES 2603430A1
- Authority
- ES
- Spain
- Prior art keywords
- receptacle
- bottle
- boom
- mouth
- tip
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title abstract 2
- 238000001514 detection method Methods 0.000 title 1
- 230000001360 synchronised effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D39/00—Refuelling during flight
- B64D39/06—Connecting hose to aircraft; Disconnecting hose therefrom
-
- 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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
- G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D39/00—Refuelling during flight
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
- G01S17/88—Lidar systems specially adapted for specific applications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
- G01S17/88—Lidar systems specially adapted for specific applications
- G01S17/93—Lidar systems specially adapted for specific applications for anti-collision purposes
- G01S17/933—Lidar systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T7/00—Image analysis
- G06T7/20—Analysis of motion
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S2205/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S2205/001—Transmission of position information to remote stations
- G01S2205/002—Transmission of position information to remote stations for traffic control, mobile tracking, guidance, surveillance or anti-collision
- G01S2205/005—Transmission of position information to remote stations for traffic control, mobile tracking, guidance, surveillance or anti-collision for aircraft positioning relative to other aircraft
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T2200/00—Indexing scheme for image data processing or generation, in general
- G06T2200/04—Indexing scheme for image data processing or generation, in general involving 3D image data
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T2207/00—Indexing scheme for image analysis or image enhancement
- G06T2207/30—Subject of image; Context of image processing
- G06T2207/30212—Military
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Electromagnetism (AREA)
- Multimedia (AREA)
- Computer Vision & Pattern Recognition (AREA)
- Theoretical Computer Science (AREA)
- Automation & Control Theory (AREA)
- Length Measuring Devices By Optical Means (AREA)
- Image Analysis (AREA)
- Image Processing (AREA)
Abstract
Sistema y procedimiento de detección de punta del botalón volador y boca de receptáculo para repostaje aéreo con botalón. Sistema de detección de la punta de la pértiga del botalón volador de un tanquero y de la boca del receptáculo del receptor para contacto semiautomático o automático para repostaje en vuelo con botalón, que asegura proporcionar al sistema de control del botalón del tanquero, información robusta, fiable y simultánea en tiempo real, del extremo de su pértiga y de la boca del receptáculo del receptor, en cada instante. Para ello el sistema cuenta con: 1) unos emisores de luz montados en la punta de su pértiga, 2) unos emisores de luz montados en el contorno del receptáculo del avión receptor, 3) un subsistema de procesamiento y 4) dos cámaras 3D, una cámara TOF, sincronizada con un emisor de luz y una cámara adicional junto con un emisor de luz estructurada generada con un lente de tipo DOE.
Description
Claims (1)
-
imagen1 imagen2 imagen3 imagen4 imagen5 imagen6 imagen7
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201630480A ES2603430B2 (es) | 2016-04-18 | 2016-04-18 | Sistema de detección y procedimiento de contacto de punta del botalón volador y boca del receptáculo para operaciones de repostaje aéreo con botalón |
US16/094,806 US11034462B2 (en) | 2016-04-18 | 2017-04-11 | Detection system and method for making contact between the tip of a flying boom and the mouth of a receptacle for aerial refuelling operations with a boom |
AU2017252334A AU2017252334B2 (en) | 2016-04-18 | 2017-04-11 | Detection system and method for making contact between the tip of a flying boom and the mouth of a receptacle for aerial refuelling operations with a boom |
PCT/ES2017/070227 WO2017182686A1 (es) | 2016-04-18 | 2017-04-11 | Sistema de detección y procedimiento de contacto de punta del botalón volador y boca del receptáculo para operaciones de repostaje aéreo con botalón |
CN201780032197.9A CN109416547A (zh) | 2016-04-18 | 2017-04-11 | 用于利用桁杆进行空中加油操作在飞桁尖端与受油器口之间形成接触的检测系统和方法 |
EP17785501.2A EP3444697A4 (en) | 2016-04-18 | 2017-04-11 | DETECTION SYSTEM AND METHOD OF SWING ARM TIP CONTACT AND RECEPTACLE ORIFICE FOR AIR SUPPLY OPERATIONS WITH ARMS |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES201630480A ES2603430B2 (es) | 2016-04-18 | 2016-04-18 | Sistema de detección y procedimiento de contacto de punta del botalón volador y boca del receptáculo para operaciones de repostaje aéreo con botalón |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2603430A1 true ES2603430A1 (es) | 2017-02-27 |
ES2603430B2 ES2603430B2 (es) | 2017-10-11 |
Family
ID=58064386
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES201630480A Active ES2603430B2 (es) | 2016-04-18 | 2016-04-18 | Sistema de detección y procedimiento de contacto de punta del botalón volador y boca del receptáculo para operaciones de repostaje aéreo con botalón |
Country Status (6)
Country | Link |
---|---|
US (1) | US11034462B2 (es) |
EP (1) | EP3444697A4 (es) |
CN (1) | CN109416547A (es) |
AU (1) | AU2017252334B2 (es) |
ES (1) | ES2603430B2 (es) |
WO (1) | WO2017182686A1 (es) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10632622B2 (en) * | 2017-12-27 | 2020-04-28 | National Chung Shan Institute Of Science And Technology | Error compensation device and error compensation method |
US11022972B2 (en) * | 2019-07-31 | 2021-06-01 | Bell Textron Inc. | Navigation system with camera assist |
CN113420031B (zh) * | 2021-06-30 | 2024-03-01 | 中国航空油料有限责任公司 | 航油数据发布系统及航油数据发布方法 |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5530650A (en) * | 1992-10-28 | 1996-06-25 | Mcdonnell Douglas Corp. | Computer imaging system and method for remote in-flight aircraft refueling |
US5904729A (en) * | 1997-03-04 | 1999-05-18 | The Boeing Company | Automated director light system for aerial refueling operations |
WO2001002875A2 (en) * | 1999-06-21 | 2001-01-11 | Lockheed Martin Corporation | System and method for locating and maintaining objects in free space |
US20030205643A1 (en) * | 2002-05-01 | 2003-11-06 | Von Thal German | Boom load alleviation using visual means |
US20030209633A1 (en) * | 2002-05-10 | 2003-11-13 | Thal German Von | Distance measuring using passive visual means |
US6966525B1 (en) * | 2004-06-28 | 2005-11-22 | The Boeing Company | In-flight refueling system, alignment system, and method for automatic alignment and engagement of an in-flight refueling boom |
US20120261516A1 (en) * | 2011-04-15 | 2012-10-18 | Patrick Gilliland | Ladar sensor for landing, docking and approach |
US20130168497A1 (en) * | 2012-01-04 | 2013-07-04 | Israel Aerospace Industries Ltd. | Systems and methods for air vehicles |
US20160023775A1 (en) * | 2012-08-09 | 2016-01-28 | The Boeing Company | Refueling boom control system |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3475001A (en) * | 1967-04-24 | 1969-10-28 | Schulz Tool & Mfg Co | Aerial refueling probe nozzle |
US7036770B2 (en) * | 2003-07-25 | 2006-05-02 | The Boeing Company | Methods and apparatus for illumination of refueling hoses |
US20100217526A1 (en) * | 2009-02-26 | 2010-08-26 | Lockheed Martin Corporation | Method for simple optical autonomous refueling system |
CN101898640A (zh) * | 2010-03-15 | 2010-12-01 | 王雪松 | 直升机空中受油装置 |
US9933521B2 (en) * | 2014-04-14 | 2018-04-03 | The Boeing Company | Aerial positioning systems and methods |
CN105083571A (zh) * | 2015-09-08 | 2015-11-25 | 天津市天舞科技有限公司 | 一种可转动桁杆式直升机空中受油装置 |
CN105383702B (zh) * | 2015-12-11 | 2017-08-25 | 中国航空工业集团公司西安航空计算技术研究所 | 一种空中加油桁杆控制计算机系统的模态切换方法 |
-
2016
- 2016-04-18 ES ES201630480A patent/ES2603430B2/es active Active
-
2017
- 2017-04-11 CN CN201780032197.9A patent/CN109416547A/zh active Pending
- 2017-04-11 WO PCT/ES2017/070227 patent/WO2017182686A1/es active Application Filing
- 2017-04-11 AU AU2017252334A patent/AU2017252334B2/en active Active
- 2017-04-11 US US16/094,806 patent/US11034462B2/en active Active
- 2017-04-11 EP EP17785501.2A patent/EP3444697A4/en not_active Ceased
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5530650A (en) * | 1992-10-28 | 1996-06-25 | Mcdonnell Douglas Corp. | Computer imaging system and method for remote in-flight aircraft refueling |
US5904729A (en) * | 1997-03-04 | 1999-05-18 | The Boeing Company | Automated director light system for aerial refueling operations |
WO2001002875A2 (en) * | 1999-06-21 | 2001-01-11 | Lockheed Martin Corporation | System and method for locating and maintaining objects in free space |
US20030205643A1 (en) * | 2002-05-01 | 2003-11-06 | Von Thal German | Boom load alleviation using visual means |
US20030209633A1 (en) * | 2002-05-10 | 2003-11-13 | Thal German Von | Distance measuring using passive visual means |
US6966525B1 (en) * | 2004-06-28 | 2005-11-22 | The Boeing Company | In-flight refueling system, alignment system, and method for automatic alignment and engagement of an in-flight refueling boom |
US20120261516A1 (en) * | 2011-04-15 | 2012-10-18 | Patrick Gilliland | Ladar sensor for landing, docking and approach |
US20130168497A1 (en) * | 2012-01-04 | 2013-07-04 | Israel Aerospace Industries Ltd. | Systems and methods for air vehicles |
US20160023775A1 (en) * | 2012-08-09 | 2016-01-28 | The Boeing Company | Refueling boom control system |
Also Published As
Publication number | Publication date |
---|---|
US20190118963A1 (en) | 2019-04-25 |
ES2603430B2 (es) | 2017-10-11 |
EP3444697A4 (en) | 2019-10-16 |
WO2017182686A1 (es) | 2017-10-26 |
US11034462B2 (en) | 2021-06-15 |
AU2017252334A1 (en) | 2018-11-15 |
AU2017252334B2 (en) | 2022-03-17 |
CN109416547A (zh) | 2019-03-01 |
EP3444697A1 (en) | 2019-02-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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