FR3037412B1 - Procede et dispositif de surveillance automatique d'une approche autonome d'un aeronef. - Google Patents

Procede et dispositif de surveillance automatique d'une approche autonome d'un aeronef. Download PDF

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Publication number
FR3037412B1
FR3037412B1 FR1555309A FR1555309A FR3037412B1 FR 3037412 B1 FR3037412 B1 FR 3037412B1 FR 1555309 A FR1555309 A FR 1555309A FR 1555309 A FR1555309 A FR 1555309A FR 3037412 B1 FR3037412 B1 FR 3037412B1
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FR
France
Prior art keywords
limit
aircraft
alert
depending
protection
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Active
Application number
FR1555309A
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English (en)
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FR3037412A1 (fr
Inventor
Yohann Roux
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
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Airbus Operations SAS
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Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1555309A priority Critical patent/FR3037412B1/fr
Priority to US15/181,224 priority patent/US9904658B2/en
Publication of FR3037412A1 publication Critical patent/FR3037412A1/fr
Application granted granted Critical
Publication of FR3037412B1 publication Critical patent/FR3037412B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/10—Complex mathematical operations
    • G06F17/11—Complex mathematical operations for solving equations, e.g. nonlinear equations, general mathematical optimization problems
    • 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
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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]
    • G08G5/02—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

Abstract

- Le dispositif (1) comporte une unité de calcul (8) pour calculer, en temps réel, une première limite dépendant d'une hauteur de décision entrée par un pilote et une seconde limite dépendant de la hauteur courante de l'aéronef et pour sélectionner, comme limite d'alerte, la valeur maximale entre la première limite et la seconde limite, une unité de calcul (9) pour calculer, en temps réel, une limite de protection dépendant de performances de l'aéronef, une unité de comparaison (10) pour comparer la limite de protection à la limite d'alerte, et une unité d'alerte (13) pour émettre un signal d'alerte si la limite de protection est supérieure à la limite d'alerte.
FR1555309A 2015-06-11 2015-06-11 Procede et dispositif de surveillance automatique d'une approche autonome d'un aeronef. Active FR3037412B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1555309A FR3037412B1 (fr) 2015-06-11 2015-06-11 Procede et dispositif de surveillance automatique d'une approche autonome d'un aeronef.
US15/181,224 US9904658B2 (en) 2015-06-11 2016-06-13 Method and device for automatically monitoring a self-contained approach of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1555309A FR3037412B1 (fr) 2015-06-11 2015-06-11 Procede et dispositif de surveillance automatique d'une approche autonome d'un aeronef.

Publications (2)

Publication Number Publication Date
FR3037412A1 FR3037412A1 (fr) 2016-12-16
FR3037412B1 true FR3037412B1 (fr) 2021-02-12

Family

ID=54545207

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1555309A Active FR3037412B1 (fr) 2015-06-11 2015-06-11 Procede et dispositif de surveillance automatique d'une approche autonome d'un aeronef.

Country Status (2)

Country Link
US (1) US9904658B2 (fr)
FR (1) FR3037412B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9734728B2 (en) * 2015-08-20 2017-08-15 Honeywell International Inc. Systems and methods for destination selection for vehicle indications and alerts
CN112706933B (zh) * 2020-10-26 2022-08-30 中国商用飞机有限责任公司 确定和显示自动飞行进近及着陆能力的系统和方法
US20220365224A1 (en) * 2021-05-17 2022-11-17 Reliable Robotics Corporation Radar altimeter augmented receiver autonomous integrity monitoring in aircraft

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6856905B2 (en) * 2003-04-29 2005-02-15 Garmin At, Inc. Systems and methods for fault detection and exclusion in navigational systems
FR2896073B1 (fr) * 2006-01-11 2008-02-08 Airbus France Sas Systeme de pilotage d'un aeronef, au moins pour piloter l'aeronef lors d'une approche autonome en vue d'un atterrissage.
FR2904706B1 (fr) * 2006-08-02 2014-06-06 Airbus France Procede et dispositif pour determiner une hauteur de decision lors d'une approche autonome d'un aeronef.
FR2944888B1 (fr) * 2009-04-28 2012-03-30 Thales Sa Procede d'aide a la navigation pour la determination de la trajectoire d'un aeronef
US8630756B2 (en) * 2011-04-12 2014-01-14 The Boeing Company Airplane position assurance monitor
US9354078B2 (en) * 2012-09-12 2016-05-31 Honeywell International Inc. Methods and systems for indicating whether an aircraft is within distance and altitude criteria for an IFR procedure turn
US9704405B2 (en) * 2014-06-12 2017-07-11 Honeywell International Inc. Aircraft display systems and methods for providing an aircraft display for use with airport departure and arrival procedures
US9916765B2 (en) * 2015-11-04 2018-03-13 Honeywell International Inc. Aircraft systems and methods for providing landing approach alerts

Also Published As

Publication number Publication date
US20160362192A1 (en) 2016-12-15
US9904658B2 (en) 2018-02-27
FR3037412A1 (fr) 2016-12-16

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