FR3038380B1 - Procede et systeme d'affichage de contraintes verticales d'un aeronef, produit programme d'ordinateur et aeronef associes - Google Patents

Procede et systeme d'affichage de contraintes verticales d'un aeronef, produit programme d'ordinateur et aeronef associes

Info

Publication number
FR3038380B1
FR3038380B1 FR1501417A FR1501417A FR3038380B1 FR 3038380 B1 FR3038380 B1 FR 3038380B1 FR 1501417 A FR1501417 A FR 1501417A FR 1501417 A FR1501417 A FR 1501417A FR 3038380 B1 FR3038380 B1 FR 3038380B1
Authority
FR
France
Prior art keywords
aircraft
computer program
program product
vertical constraints
displaying vertical
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
FR1501417A
Other languages
English (en)
Other versions
FR3038380A1 (fr
Inventor
Matthieu Claybrough
Bruno Aymeric
Sylvain Lissajoux
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 FR1501417A priority Critical patent/FR3038380B1/fr
Priority to CA2934851A priority patent/CA2934851A1/fr
Priority to BR102016015421A priority patent/BR102016015421A2/pt
Priority to US15/201,258 priority patent/US10235891B2/en
Priority to CN201610519374.3A priority patent/CN106325293A/zh
Publication of FR3038380A1 publication Critical patent/FR3038380A1/fr
Application granted granted Critical
Publication of FR3038380B1 publication Critical patent/FR3038380B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0065—Navigation or guidance aids for a single aircraft for taking-off
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • 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
    • 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
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01—Head-up displays
    • G02B27/0101—Head-up displays characterised by optical features
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01—Head-up displays
    • G02B27/0101—Head-up displays characterised by optical features
    • G02B2027/0141—Head-up displays characterised by optical features characterised by the informative content of the display
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01—Head-up displays
    • G02B27/0179—Display position adjusting means not related to the information to be displayed
    • G02B2027/0183—Adaptation to parameters characterising the motion of the vehicle

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)
  • Optics & Photonics (AREA)
  • Traffic Control Systems (AREA)
FR1501417A 2015-07-03 2015-07-03 Procede et systeme d'affichage de contraintes verticales d'un aeronef, produit programme d'ordinateur et aeronef associes Active FR3038380B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1501417A FR3038380B1 (fr) 2015-07-03 2015-07-03 Procede et systeme d'affichage de contraintes verticales d'un aeronef, produit programme d'ordinateur et aeronef associes
CA2934851A CA2934851A1 (fr) 2015-07-03 2016-06-29 Procede et systeme d'affichage de contraintes verticales d'un aeronef, produit programme d'ordinateur et aeronef associes
BR102016015421A BR102016015421A2 (pt) 2015-07-03 2016-06-30 processo e sistema de exibição de tensões verticais de uma aeronave, produto programa de computador e aeronave associados
US15/201,258 US10235891B2 (en) 2015-07-03 2016-07-01 Method and device for displaying vertical constraints of an aircraft, associated computer program product and aircraft
CN201610519374.3A CN106325293A (zh) 2015-07-03 2016-07-04 飞行器纵向约束显示方法和系统，计算机程序产品和飞行器

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1501417A FR3038380B1 (fr) 2015-07-03 2015-07-03 Procede et systeme d'affichage de contraintes verticales d'un aeronef, produit programme d'ordinateur et aeronef associes

Publications (2)

Publication Number Publication Date
FR3038380A1 FR3038380A1 (fr) 2017-01-06
FR3038380B1 true FR3038380B1 (fr) 2017-08-18

Family

ID=54291345

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1501417A Active FR3038380B1 (fr) 2015-07-03 2015-07-03 Procede et systeme d'affichage de contraintes verticales d'un aeronef, produit programme d'ordinateur et aeronef associes

Country Status (5)

Country Link
US (1) US10235891B2 (fr)
CN (1) CN106325293A (fr)
BR (1) BR102016015421A2 (fr)
CA (1) CA2934851A1 (fr)
FR (1) FR3038380B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10388170B2 (en) 2017-08-14 2019-08-20 Honeywell International Inc. Speed-constrained flight management methods and systems
FR3082304B1 (fr) * 2018-06-12 2020-06-05 Thales Procede et dispositif electronique de gestion de l'affichage d'un plan de vol d'un aeronef, programme d'ordinateur et systeme electronique d'affichage associes
FR3086074B1 (fr) * 2018-09-18 2020-08-14 Airbus Operations Sas Systeme et procede d'aide au pilotage d'un aeronef
FR3089497A1 (fr) * 2018-12-10 2020-06-12 Airbus Operations Procédé et dispositif d’aide au pilotage d’un aéronef lors d’une approche d’une piste d’atterrissage en vue d’un atterrissage
CN110069070B (zh) * 2019-05-08 2022-01-18 成都高威节能科技有限公司 一种提高大型飞机起飞过程安全性的方法
CN110113094B (zh) * 2019-05-09 2021-08-13 西安爱生技术集团公司 一种升空通信中继无人机通视计算方法
CN115585814B (zh) * 2022-12-12 2023-03-21 北京理工大学 一种基于沉降机制的飞行器变尺度地形跟随方法
CN115979157B (zh) * 2022-12-31 2023-09-12 同济大学 一种基于远距激光测振的道面结构性能评价方法及系统

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2725803B1 (fr) * 1994-10-18 1997-01-03 Sextant Avionique Dispositif optoelectronique d'assistance au pilotage d'un aeronef
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
US7783393B2 (en) * 2004-06-30 2010-08-24 The Boeing Company Enhanced vertical situation display
FR2887329B1 (fr) * 2005-06-21 2007-08-03 Airbus France Sas Procede et dispositif d'affichage pour un aeronef qui suit un plan de vol
FR2943131B1 (fr) * 2009-03-12 2011-02-25 Eurocopter France Procede de determination et d'affichage d'indications de pilotage et indicateur de pilotage pour mettre en oeuvre ledit procede
FR2978589B1 (fr) * 2011-07-29 2013-08-23 Airbus Operations Sas Procede et dispositif de gestion optimisee de la trajectoire verticale d'un aeronef
US8818579B2 (en) * 2012-08-30 2014-08-26 Honeywell International Inc. Systems and methods for graphically indicating aircraft ascent and descent capabilities
FR3005727B1 (fr) * 2013-05-15 2020-03-06 Airbus Operations Procede et dispositif d'affichage de performances d'un aeronef en montee et/ou en descente.
FR3012630B1 (fr) * 2013-10-25 2016-01-01 Thales Sa Procede d'aide a la navigation pour un aeronef en descente et en approche a poussee reduite
CN104267734B (zh) * 2014-08-01 2016-11-02 北京理工大学 一种燃料最省的火星复杂地形区安全着陆轨迹生成方法

Also Published As

Publication number Publication date
CA2934851A1 (fr) 2017-01-03
BR102016015421A2 (pt) 2017-01-24
FR3038380A1 (fr) 2017-01-06
US10235891B2 (en) 2019-03-19
CN106325293A (zh) 2017-01-11
US20170004713A1 (en) 2017-01-05

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