FR3111710B1 - Procédé et système d’estimation d’une déviation angulaire d’un axe de guidage de référence, d’une position et d’une vitesse d’un aéronef. - Google Patents

Procédé et système d’estimation d’une déviation angulaire d’un axe de guidage de référence, d’une position et d’une vitesse d’un aéronef. Download PDF

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Publication number
FR3111710B1
FR3111710B1 FR2006443A FR2006443A FR3111710B1 FR 3111710 B1 FR3111710 B1 FR 3111710B1 FR 2006443 A FR2006443 A FR 2006443A FR 2006443 A FR2006443 A FR 2006443A FR 3111710 B1 FR3111710 B1 FR 3111710B1
Authority
FR
France
Prior art keywords
estimating
aircraft
speed
angular deviation
guidance axis
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
Application number
FR2006443A
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English (en)
Other versions
FR3111710A1 (fr
Inventor
Thierry Bourret
Guillaume Alcalay
Michel Padovani
Imad Lebbos
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus SAS
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 Airbus Operations SAS, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR2006443A priority Critical patent/FR3111710B1/fr
Priority to CN202110647800.2A priority patent/CN113823126A/zh
Priority to US17/345,454 priority patent/US11747170B2/en
Publication of FR3111710A1 publication Critical patent/FR3111710A1/fr
Application granted granted Critical
Publication of FR3111710B1 publication Critical patent/FR3111710B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • 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
    • 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
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
    • 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
    • G01C21/20—Instruments for performing navigational calculations
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D21/00—Measuring or testing not otherwise provided for
    • G01D21/02—Measuring two or more variables by means not covered by a single other subclass
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • 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
    • G01S5/0257—Hybrid positioning
    • G01S5/0263—Hybrid positioning by combining or switching between positions derived from two or more separate positioning systems
    • 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
    • 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
    • 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
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G01S19/48—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
    • 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
    • G01S2205/01—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations specially adapted for specific applications
    • G01S2205/03—Airborne
    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/02—Registering or indicating driving, working, idle, or waiting time only

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)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)

Abstract

- Procédé et système d’estimation d’une déviation angulaire d’un axe de guidage de référence, d’une position et d’une vitesse d’un aéronef. - Le système (1) comprend un module de collecte d’écart (2) mesuré par un module de mesure (21), un module de collecte de vecteur position (3) mesuré par un module de mesure de vecteur position (31), un module de collecte de vecteur vitesse (4), un module d’estimation de la déviation angulaire d’un axe de guidage de référence par rapport à l’axe d’approche de la piste d’atterrissage, d’estimation de la position de l’aéronef par rapport à la piste d’atterrissage et d’estimation de la vitesse de l’aéronef par rapport à la piste d’atterrissage. Figure pour l'abrégé : Fig. 1
FR2006443A 2020-06-19 2020-06-19 Procédé et système d’estimation d’une déviation angulaire d’un axe de guidage de référence, d’une position et d’une vitesse d’un aéronef. Active FR3111710B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR2006443A FR3111710B1 (fr) 2020-06-19 2020-06-19 Procédé et système d’estimation d’une déviation angulaire d’un axe de guidage de référence, d’une position et d’une vitesse d’un aéronef.
CN202110647800.2A CN113823126A (zh) 2020-06-19 2021-06-10 用于估计与参考引导轴线的角偏差、飞行器的位置和速度的方法和系统
US17/345,454 US11747170B2 (en) 2020-06-19 2021-06-11 Method and system for estimating an angular deviation from a reference guidance axis, a position and a velocity of an aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2006443A FR3111710B1 (fr) 2020-06-19 2020-06-19 Procédé et système d’estimation d’une déviation angulaire d’un axe de guidage de référence, d’une position et d’une vitesse d’un aéronef.
FR2006443 2020-06-19

Publications (2)

Publication Number Publication Date
FR3111710A1 FR3111710A1 (fr) 2021-12-24
FR3111710B1 true FR3111710B1 (fr) 2022-12-09

Family

ID=72470544

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2006443A Active FR3111710B1 (fr) 2020-06-19 2020-06-19 Procédé et système d’estimation d’une déviation angulaire d’un axe de guidage de référence, d’une position et d’une vitesse d’un aéronef.

Country Status (3)

Country Link
US (1) US11747170B2 (fr)
CN (1) CN113823126A (fr)
FR (1) FR3111710B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3147420A1 (fr) * 2023-03-30 2024-10-04 Airbus Operations Procédé et dispositif d’estimation d’une position et d’une vitesse d’un aéronef lors d’une phase d’approche permettant un atterrissage automatique.
CN118094107B (zh) * 2024-04-08 2024-06-21 北京华力兴科技发展有限责任公司 异常数据检测方法及异常数据诊断器、射线测厚仪

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6178363B1 (en) 1998-12-22 2001-01-23 The Boeing Company Inertially augmented GPS landing system
US6522266B1 (en) * 2000-05-17 2003-02-18 Honeywell, Inc. Navigation system, method and software for foot travel
US8958932B2 (en) * 2013-02-11 2015-02-17 The Boeing Company Methods and apparatus to mitigate instrument landing system overflight interference
US9098999B2 (en) * 2013-09-13 2015-08-04 The Boeing Company Systems and methods for assuring the accuracy of a synthetic runway presentation
KR101715336B1 (ko) * 2014-10-31 2017-03-10 한국항공우주연구원 항공기 착륙을 위한 통합 착륙 수신 장치 및 그 제어 방법
FR3038045B1 (fr) * 2015-06-24 2019-05-31 Dassault Aviation Systeme d'affichage d'un aeronef comprenant un symbole de guidage d'arrondi et procede associe
US11104446B2 (en) * 2016-07-01 2021-08-31 Textron Innovations Inc. Line replaceable propulsion assemblies for aircraft
US10386202B2 (en) * 2017-02-17 2019-08-20 The Charles Stark Draper Laboratory, Inc. Systems and methods for determining quality and integrity of source information to determine navigation information of an object

Also Published As

Publication number Publication date
FR3111710A1 (fr) 2021-12-24
US11747170B2 (en) 2023-09-05
CN113823126A (zh) 2021-12-21
US20210396545A1 (en) 2021-12-23

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