MX359587B - Metodo para guiar una aeronave. - Google Patents
Metodo para guiar una aeronave.Info
- Publication number
- MX359587B MX359587B MX2016013895A MX2016013895A MX359587B MX 359587 B MX359587 B MX 359587B MX 2016013895 A MX2016013895 A MX 2016013895A MX 2016013895 A MX2016013895 A MX 2016013895A MX 359587 B MX359587 B MX 359587B
- Authority
- MX
- Mexico
- Prior art keywords
- aircraft
- platform
- relative location
- reference path
- confidence index
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/51—Navigation or guidance aids for control when on the ground, e.g. taxiing or rolling
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/74—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems
- G01S13/76—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems wherein pulse-type signals are transmitted
- G01S13/765—Systems using reradiation of radio waves, e.g. secondary radar systems; Analogous systems wherein pulse-type signals are transmitted with exchange of information between interrogator and responder
-
- 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
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/0205—Details
- G01S5/0244—Accuracy or reliability of position solution or of measurements contributing thereto
-
- 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
-
- 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
- G05D1/0083—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots to help an aircraft pilot in the rolling phase
-
- 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
- G05D1/02—Control of position or course in two dimensions
- G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F18/00—Pattern recognition
- G06F18/20—Analysing
- G06F18/22—Matching criteria, e.g. proximity measures
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T7/00—Image analysis
- G06T7/70—Determining position or orientation of objects or cameras
- G06T7/73—Determining position or orientation of objects or cameras using feature-based methods
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
- G08G5/21—Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft
-
- G—PHYSICS
- G06—COMPUTING OR CALCULATING; COUNTING
- G06V—IMAGE OR VIDEO RECOGNITION OR UNDERSTANDING
- G06V20/00—Scenes; Scene-specific elements
- G06V20/50—Context or environment of the image
- G06V20/56—Context or environment of the image exterior to a vehicle by using sensors mounted on the vehicle
Landscapes
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Theoretical Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Computer Vision & Pattern Recognition (AREA)
- Data Mining & Analysis (AREA)
- Artificial Intelligence (AREA)
- Evolutionary Biology (AREA)
- Evolutionary Computation (AREA)
- General Engineering & Computer Science (AREA)
- Bioinformatics & Cheminformatics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Bioinformatics & Computational Biology (AREA)
- Multimedia (AREA)
- Traffic Control Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
- Navigation (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
La invención se refiere a un método para guiar una aeronave a lo largo de una trayectoria de referencia en una plataforma terrestre, dicha aeronave porta por lo menos un detector para detectar una pluralidad de indicadores en tierra, dicho método comprende: a) determinar (E1) zonas de incertidumbre geométricamente complejas de la plataforma usando un mapa de la plataforma, b) seleccionar (E2) por lo menos un indicador cerca de una de dichas zonas de incertidumbre, c) estimar (E3) la ubicación relativa de la aeronave con relación a dicha trayectoria de referencia usando datos relacionados con los indicadores seleccionados transmitidos por los detectores, d) calcular (E4) un índice de confianza relacionado con la ubicación relativa estimada usando los indicadores seleccionados, e) comparar (E5) el índice de confianza calculado con un límite predeterminado, f) cuando el índice de confianza calculado sea mayor que un límite predeterminado, guiar (E6) a la aeronave a lo largo de la trayectoria de referencia con base en la ubicación relativa estimada.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1453590A FR3020172B1 (fr) | 2014-04-22 | 2014-04-22 | Procede de guidage d'un aeronef |
| PCT/EP2015/058654 WO2015162152A1 (fr) | 2014-04-22 | 2015-04-22 | Procédé de guidage d'un aéronef |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| MX2016013895A MX2016013895A (es) | 2017-06-29 |
| MX359587B true MX359587B (es) | 2018-10-02 |
Family
ID=51063658
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| MX2016013895A MX359587B (es) | 2014-04-22 | 2015-04-22 | Metodo para guiar una aeronave. |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US9990855B2 (es) |
| EP (1) | EP3134791B1 (es) |
| CN (1) | CN106462163B (es) |
| BR (1) | BR112016024640A2 (es) |
| ES (1) | ES2964768T3 (es) |
| FR (1) | FR3020172B1 (es) |
| IL (1) | IL248454B (es) |
| MX (1) | MX359587B (es) |
| PL (1) | PL3134791T3 (es) |
| RU (1) | RU2016145426A (es) |
| WO (1) | WO2015162152A1 (es) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3020172B1 (fr) * | 2014-04-22 | 2016-05-06 | Sagem Defense Securite | Procede de guidage d'un aeronef |
| FR3044153B1 (fr) * | 2015-11-19 | 2017-11-10 | Airbus | Procede de pilotage automatique d'un aeronef au sol et dispositif pour sa mise en oeuvre |
| FR3051264B1 (fr) * | 2016-05-13 | 2018-04-27 | Robert Schegerin | Pilotage automatique d'un aeronef a deconnexion differee |
| US20180018887A1 (en) * | 2016-07-18 | 2018-01-18 | Honeywell International Inc. | Routing aircraft ground movements at an airport |
| FR3062835B1 (fr) * | 2017-02-10 | 2019-04-26 | Valeo Schalter Und Sensoren Gmbh | Procede et systeme de determination d'un indice de confiance associe a une caracteristique d'une voie de circulation |
| CN108778930A (zh) * | 2017-09-30 | 2018-11-09 | 深圳市大疆创新科技有限公司 | 飞行器安全保护方法、设备、飞行器及无人机系统 |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5172317A (en) * | 1988-08-10 | 1992-12-15 | Honda Giken Kogyo Kabushiki Kaisha | Automatic travelling apparatus |
| US6038498A (en) * | 1997-10-15 | 2000-03-14 | Dassault Aviation | Apparatus and mehod for aircraft monitoring and control including electronic check-list management |
| FR2808588B1 (fr) * | 2000-05-05 | 2002-08-09 | Thomson Csf | Procede et dispositif de determination de la position d'un vehicule par rapport a une trajectoire ideale |
| FR2911713B1 (fr) * | 2007-01-19 | 2014-03-21 | Thales Sa | Dispositif et procede de mesure de parametres dynamiques d'un aeronef evoluant sur une zone aeroportuaire |
| US8380367B2 (en) * | 2009-03-26 | 2013-02-19 | The University Of North Dakota | Adaptive surveillance and guidance system for vehicle collision avoidance and interception |
| FR2959052B1 (fr) * | 2010-04-16 | 2012-12-28 | Thales Sa | Dispositif d'assistance embarque au suivi d'une route aeroportuaire par un aeronef |
| CN102169540B (zh) * | 2011-03-28 | 2013-03-13 | 汉王科技股份有限公司 | 基于拍摄仪的点读定位方法和装置 |
| KR101193115B1 (ko) * | 2011-10-07 | 2012-10-19 | 한국항공우주산업 주식회사 | 3d 전자 지도 시스템 |
| KR20130065126A (ko) * | 2011-12-09 | 2013-06-19 | 한국전자통신연구원 | 이동체의 경로 설정 장치 및 방법 |
| CN103985214A (zh) * | 2014-04-15 | 2014-08-13 | 中国民航大学 | 基于ccd与rfid电子标签的飞机防护系统 |
| FR3020172B1 (fr) * | 2014-04-22 | 2016-05-06 | Sagem Defense Securite | Procede de guidage d'un aeronef |
-
2014
- 2014-04-22 FR FR1453590A patent/FR3020172B1/fr active Active
-
2015
- 2015-04-22 MX MX2016013895A patent/MX359587B/es active IP Right Grant
- 2015-04-22 EP EP15716850.1A patent/EP3134791B1/fr active Active
- 2015-04-22 RU RU2016145426A patent/RU2016145426A/ru not_active Application Discontinuation
- 2015-04-22 WO PCT/EP2015/058654 patent/WO2015162152A1/fr not_active Ceased
- 2015-04-22 BR BR112016024640A patent/BR112016024640A2/pt not_active Application Discontinuation
- 2015-04-22 CN CN201580021771.1A patent/CN106462163B/zh active Active
- 2015-04-22 PL PL15716850.1T patent/PL3134791T3/pl unknown
- 2015-04-22 US US15/305,634 patent/US9990855B2/en active Active
- 2015-04-22 ES ES15716850T patent/ES2964768T3/es active Active
-
2016
- 2016-10-23 IL IL248454A patent/IL248454B/en active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| MX2016013895A (es) | 2017-06-29 |
| CN106462163A (zh) | 2017-02-22 |
| RU2016145426A (ru) | 2018-05-23 |
| EP3134791B1 (fr) | 2023-09-13 |
| PL3134791T3 (pl) | 2024-04-02 |
| US9990855B2 (en) | 2018-06-05 |
| BR112016024640A2 (pt) | 2017-08-15 |
| ES2964768T3 (es) | 2024-04-09 |
| EP3134791A1 (fr) | 2017-03-01 |
| US20170046963A1 (en) | 2017-02-16 |
| IL248454A0 (en) | 2016-11-30 |
| IL248454B (en) | 2019-07-31 |
| FR3020172A1 (fr) | 2015-10-23 |
| WO2015162152A1 (fr) | 2015-10-29 |
| RU2016145426A3 (es) | 2018-11-19 |
| CN106462163B (zh) | 2019-11-05 |
| FR3020172B1 (fr) | 2016-05-06 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG | Grant or registration |