FR3018383B1 - Procede et dispositif de determination de parametres de navigation d'un aeronef lors d'une phase d'atterrissage. - Google Patents
Procede et dispositif de determination de parametres de navigation d'un aeronef lors d'une phase d'atterrissage.Info
- Publication number
- FR3018383B1 FR3018383B1 FR1451848A FR1451848A FR3018383B1 FR 3018383 B1 FR3018383 B1 FR 3018383B1 FR 1451848 A FR1451848 A FR 1451848A FR 1451848 A FR1451848 A FR 1451848A FR 3018383 B1 FR3018383 B1 FR 3018383B1
- Authority
- FR
- France
- Prior art keywords
- aircraft during
- navigation parameters
- landing phase
- determining navigation
- determining
- 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.)
- Active
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
- G01C23/005—Flight directors
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/165—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
- G01C21/1656—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments with passive imaging devices, e.g. cameras
-
- 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
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
- G01S19/14—Receivers specially adapted for specific applications
- G01S19/15—Aircraft landing systems
-
- 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
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
- G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Computer Networks & Wireless Communication (AREA)
- Navigation (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1451848A FR3018383B1 (fr) | 2014-03-07 | 2014-03-07 | Procede et dispositif de determination de parametres de navigation d'un aeronef lors d'une phase d'atterrissage. |
US14/637,554 US9593963B2 (en) | 2014-03-07 | 2015-03-04 | Method and a device for determining navigation parameters of an aircraft during a landing phase |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1451848A FR3018383B1 (fr) | 2014-03-07 | 2014-03-07 | Procede et dispositif de determination de parametres de navigation d'un aeronef lors d'une phase d'atterrissage. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3018383A1 FR3018383A1 (fr) | 2015-09-11 |
FR3018383B1 true FR3018383B1 (fr) | 2017-09-08 |
Family
ID=51210514
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1451848A Active FR3018383B1 (fr) | 2014-03-07 | 2014-03-07 | Procede et dispositif de determination de parametres de navigation d'un aeronef lors d'une phase d'atterrissage. |
Country Status (2)
Country | Link |
---|---|
US (1) | US9593963B2 (fr) |
FR (1) | FR3018383B1 (fr) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2998958B1 (fr) * | 2012-12-05 | 2019-10-18 | Thales | Procede de gestion de donnees air (air data) d'un aeronef |
FR3000196B1 (fr) * | 2012-12-21 | 2015-02-06 | Airbus Operations Sas | Dispositif de mise a disposition de valeurs de parametres de navigation d'un vehicule |
US9593962B2 (en) | 2014-10-08 | 2017-03-14 | Honeywell International Inc. | Systems and methods for attitude fault detection based on integrated GNSS/inertial hybrid filter residuals |
US9435661B2 (en) * | 2014-10-08 | 2016-09-06 | Honeywell International Inc. | Systems and methods for attitude fault detection based on air data and aircraft control settings |
US9832085B1 (en) * | 2015-01-20 | 2017-11-28 | Mehdi Malboubi | System for estimating unknown attributes of interest in the under-determined inverse problem and a process of accomplishing the same |
KR101784955B1 (ko) | 2016-05-04 | 2017-10-12 | 엘아이지넥스원 주식회사 | 영상 정보를 이용한 비행 속도 산출 방법 |
WO2018125333A2 (fr) * | 2016-09-22 | 2018-07-05 | The Regents Of The University Of California | Sdr destiné à une navigation au moyen des signaux lte |
DE102016222272B4 (de) * | 2016-11-14 | 2018-05-30 | Volkswagen Aktiengesellschaft | Schätzen einer Eigenposition |
CN109269511B (zh) * | 2018-11-06 | 2020-01-07 | 北京理工大学 | 未知环境下行星着陆的曲线匹配视觉导航方法 |
CN109375647A (zh) * | 2018-11-20 | 2019-02-22 | 中国航空工业集团公司西安航空计算技术研究所 | 微型多源感知计算*** |
CN109341686B (zh) * | 2018-12-04 | 2023-10-27 | 中国航空工业集团公司西安航空计算技术研究所 | 一种基于视觉-惯性紧耦合的飞行器着陆位姿估计方法 |
CN109341685B (zh) * | 2018-12-04 | 2023-06-30 | 中国航空工业集团公司西安航空计算技术研究所 | 一种基于单应变换的固定翼飞机视觉辅助着陆导航方法 |
FR3097045B1 (fr) | 2019-06-06 | 2021-05-14 | Safran Electronics & Defense | Procédé et dispositif de recalage d’une centrale inertielle d’un moyen de transport à partir d’informations délivrées par un viseur du moyen de transport |
CN111912401B (zh) * | 2020-06-30 | 2021-08-03 | 成都飞机工业(集团)有限责任公司 | 一种面向飞机大部件调姿机构工作空间求解方法 |
CN112051573B (zh) * | 2020-08-27 | 2024-06-11 | 民航空管技术装备发展有限公司 | 一种航迹处理方法及装置、存储介质 |
CN113109852B (zh) * | 2021-03-11 | 2024-03-12 | 国网江西省电力有限公司电力科学研究院 | 一种无人机进狭窄空间的路径规划方法及装置 |
CN114266103B (zh) * | 2021-09-16 | 2023-05-19 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种飞行器参数和噪声特性在线估计方法及存储介质 |
FR3139653A1 (fr) * | 2022-09-13 | 2024-03-15 | Safran Electronics & Defense | Procédé et dispositif de navigation pour un véhicule, système, véhicule, programme d'ordinateur et support d'informations associés |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6405975B1 (en) * | 1995-12-19 | 2002-06-18 | The Boeing Company | Airplane ground maneuvering camera system |
US6028624A (en) * | 1997-12-11 | 2000-02-22 | The United States Of America As Represented By The Secretary Of The Army | Method and apparatus for increased visibility through fog and other aerosols |
US6157876A (en) * | 1999-10-12 | 2000-12-05 | Honeywell International Inc. | Method and apparatus for navigating an aircraft from an image of the runway |
FR2835314B1 (fr) * | 2002-01-25 | 2004-04-30 | Airbus France | Procede de guidage d'un aeronef en phase finale d'atterrissage et dispositif correspondant |
JP4253239B2 (ja) * | 2003-10-07 | 2009-04-08 | 富士重工業株式会社 | 画像認識を用いた航法装置 |
FR2896071A1 (fr) * | 2006-01-11 | 2007-07-13 | Airbus France Sas | Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche autonome. |
FR2897840B1 (fr) * | 2006-02-27 | 2009-02-13 | Eurocopter France | Procede et dispositif de traitement et de visualisation d'informations de pilotage d'un aeronef |
FR2928021B1 (fr) * | 2008-02-25 | 2011-06-10 | Airbus France | Procede et dispositif de detection d'un aeronef environnant. |
US8284997B2 (en) * | 2009-03-11 | 2012-10-09 | Honeywell International Inc. | Vision-based vehicle navigation system and method |
US8406466B2 (en) * | 2009-12-14 | 2013-03-26 | Honeywell International Inc. | Converting aircraft enhanced vision system video to simulated real time video |
US20110282580A1 (en) * | 2010-05-11 | 2011-11-17 | Honeywell International Inc. | Method of image based navigation for precision guidance and landing |
FR2961897B1 (fr) * | 2010-06-25 | 2012-07-13 | Thales Sa | Filtre de navigation pour un systeme de navigation par correlation de terrain |
US8600589B2 (en) * | 2012-04-24 | 2013-12-03 | Exelis, Inc. | Point cloud visualization of acceptable helicopter landing zones based on 4D LIDAR |
CN104006790A (zh) * | 2013-02-21 | 2014-08-27 | 成都海存艾匹科技有限公司 | 基于视觉的飞机降落辅助装置 |
-
2014
- 2014-03-07 FR FR1451848A patent/FR3018383B1/fr active Active
-
2015
- 2015-03-04 US US14/637,554 patent/US9593963B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US9593963B2 (en) | 2017-03-14 |
US20150253150A1 (en) | 2015-09-10 |
FR3018383A1 (fr) | 2015-09-11 |
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