FR2988202B1 - Procede d'aide a la navigation pour le suivi de la performance de navigation en lineaire ou angulaire - Google Patents

Procede d'aide a la navigation pour le suivi de la performance de navigation en lineaire ou angulaire

Info

Publication number
FR2988202B1
FR2988202B1 FR1200755A FR1200755A FR2988202B1 FR 2988202 B1 FR2988202 B1 FR 2988202B1 FR 1200755 A FR1200755 A FR 1200755A FR 1200755 A FR1200755 A FR 1200755A FR 2988202 B1 FR2988202 B1 FR 2988202B1
Authority
FR
France
Prior art keywords
navigation
angular
assistance method
performance
monitoring linear
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
FR1200755A
Other languages
English (en)
Other versions
FR2988202A1 (fr
Inventor
Guilhem Putz
Christophe Caillaud
Francois Coulmeau
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.)
Thales SA
Original Assignee
Thales SA
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 Thales SA filed Critical Thales SA
Priority to FR1200755A priority Critical patent/FR2988202B1/fr
Priority to US13/797,485 priority patent/US8948939B2/en
Publication of FR2988202A1 publication Critical patent/FR2988202A1/fr
Application granted granted Critical
Publication of FR2988202B1 publication Critical patent/FR2988202B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
    • G—PHYSICS
    • 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]
    • G08G5/0017—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
FR1200755A 2012-03-13 2012-03-13 Procede d'aide a la navigation pour le suivi de la performance de navigation en lineaire ou angulaire Active FR2988202B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1200755A FR2988202B1 (fr) 2012-03-13 2012-03-13 Procede d'aide a la navigation pour le suivi de la performance de navigation en lineaire ou angulaire
US13/797,485 US8948939B2 (en) 2012-03-13 2013-03-12 Navigation assistance method for monitoring navigation performance in linear or angular mode

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1200755A FR2988202B1 (fr) 2012-03-13 2012-03-13 Procede d'aide a la navigation pour le suivi de la performance de navigation en lineaire ou angulaire

Publications (2)

Publication Number Publication Date
FR2988202A1 FR2988202A1 (fr) 2013-09-20
FR2988202B1 true FR2988202B1 (fr) 2015-05-15

Family

ID=46331411

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1200755A Active FR2988202B1 (fr) 2012-03-13 2012-03-13 Procede d'aide a la navigation pour le suivi de la performance de navigation en lineaire ou angulaire

Country Status (2)

Country Link
US (1) US8948939B2 (fr)
FR (1) FR2988202B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3017703B1 (fr) * 2014-02-14 2017-12-22 Thales Sa Procede et systeme de determination de la compatibilite d'un guidage angulaire avec une approche
FR3081580B1 (fr) 2018-05-25 2020-05-22 Thales Procede et dispositif electronique de gestion de l'affichage d'un profil de vol d'un aeronef, programme d'ordinateur et systeme electronique d'affichage associes
FR3110985A1 (fr) * 2020-05-29 2021-12-03 Airbus Interface homme-machine d’un aéronef en phase de décollage ou d’atterrissage

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3327973A (en) * 1965-06-14 1967-06-27 Lear Siegler Inc Automatic landing pitch axis control system for aircraft
US3946387A (en) * 1974-08-26 1976-03-23 The Boeing Company Method and apparatus for adjustment of modulation course patterns in a navigational system
US4170767A (en) * 1977-02-25 1979-10-09 Tanner Jesse H Visual approach system for aircraft
US5745863A (en) * 1995-09-22 1998-04-28 Honeywell Inc. Three dimensional lateral displacement display symbology which is conformal to the earth
US6320579B1 (en) * 1998-12-30 2001-11-20 Honeywell International Inc. Cockpit display having 3D flight path error symbology
US7216069B2 (en) * 2001-01-19 2007-05-08 Honeywell International, Inc. Simulated visual glideslope indicator on aircraft display
US6571155B2 (en) * 2001-07-02 2003-05-27 The Boeing Company Assembly, computer program product and method for displaying navigation performance based flight path deviation information
FR2847553B1 (fr) * 2002-11-27 2004-12-31 Eurocopter France Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segment
US6885313B2 (en) * 2003-03-26 2005-04-26 Honeywell International Inc. Graphical display for aircraft navigation
FR2854129B1 (fr) * 2003-04-28 2007-06-01 Airbus France Dispositif d'affichage dans un cockpit d'aeronef d'informations concernant le trafic environnant
US8812181B2 (en) * 2005-06-29 2014-08-19 Honeywell International Inc. Methods and systems to accurately display lateral deviation symbology in offset approaches to runways
FR2897712B1 (fr) * 2006-02-20 2008-04-04 Airbus France Sas Dispositif d'aide au pilotage d'un aeronef lors d'une phase d'approche en vue d'un atterrissage.
US8027756B2 (en) * 2006-12-07 2011-09-27 The Boeing Company Integrated approach navigation system, method, and computer program product
US8630756B2 (en) * 2011-04-12 2014-01-14 The Boeing Company Airplane position assurance monitor

Also Published As

Publication number Publication date
US20130245861A1 (en) 2013-09-19
FR2988202A1 (fr) 2013-09-20
US8948939B2 (en) 2015-02-03

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