FR2946161B1 - Procede d'elaboration continue et adaptative d'une consigne de vitesse pour la tenue d'un rta par un aeronef - Google Patents

Procede d'elaboration continue et adaptative d'une consigne de vitesse pour la tenue d'un rta par un aeronef

Info

Publication number
FR2946161B1
FR2946161B1 FR0902613A FR0902613A FR2946161B1 FR 2946161 B1 FR2946161 B1 FR 2946161B1 FR 0902613 A FR0902613 A FR 0902613A FR 0902613 A FR0902613 A FR 0902613A FR 2946161 B1 FR2946161 B1 FR 2946161B1
Authority
FR
France
Prior art keywords
rta
aircraft
holding
continuous
speed set
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
FR0902613A
Other languages
English (en)
Other versions
FR2946161A1 (fr
Inventor
Wright Benoit Dacre
Guy Deker
Xavier Blanchon
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 FR0902613A priority Critical patent/FR2946161B1/fr
Priority to US12/790,596 priority patent/US8332145B2/en
Publication of FR2946161A1 publication Critical patent/FR2946161A1/fr
Application granted granted Critical
Publication of FR2946161B1 publication Critical patent/FR2946161B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • G08G5/0026—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located on the ground
    • 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
    • G08G5/0052—Navigation or guidance aids for a single aircraft for cruising

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
FR0902613A 2009-05-29 2009-05-29 Procede d'elaboration continue et adaptative d'une consigne de vitesse pour la tenue d'un rta par un aeronef Active FR2946161B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0902613A FR2946161B1 (fr) 2009-05-29 2009-05-29 Procede d'elaboration continue et adaptative d'une consigne de vitesse pour la tenue d'un rta par un aeronef
US12/790,596 US8332145B2 (en) 2009-05-29 2010-05-28 Method for continuously and adaptively generating a speed setpoint for an aircraft to observe an RTA

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0902613A FR2946161B1 (fr) 2009-05-29 2009-05-29 Procede d'elaboration continue et adaptative d'une consigne de vitesse pour la tenue d'un rta par un aeronef

Publications (2)

Publication Number Publication Date
FR2946161A1 FR2946161A1 (fr) 2010-12-03
FR2946161B1 true FR2946161B1 (fr) 2016-08-26

Family

ID=42142719

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0902613A Active FR2946161B1 (fr) 2009-05-29 2009-05-29 Procede d'elaboration continue et adaptative d'une consigne de vitesse pour la tenue d'un rta par un aeronef

Country Status (2)

Country Link
US (1) US8332145B2 (fr)
FR (1) FR2946161B1 (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8311687B2 (en) * 2010-07-30 2012-11-13 Ge Aviation Systems Llc Method and system for vertical navigation using time-of-arrival control
US8406939B2 (en) * 2010-09-03 2013-03-26 Honeywell International Inc. Systems and methods for RTA control of multi-segment flight plans with smooth transitions
FR2973502B1 (fr) 2011-03-29 2014-01-10 Airbus Operations Sas Procede et dispositif de verification de la tenue de contraintes de temps successives par un aeronef.
FR2983619B1 (fr) * 2011-12-05 2013-11-22 Thales Sa Procede, dispositif et systeme pour garantir un espacement temporel entre un aeronef et au moins un trafic cible
FR2991094B1 (fr) 2012-05-25 2015-02-27 Thales Sa Dispositif de gestion de vol d'un aeronef adapte a la maitrise de contraintes de temps multiples et procede correspondant
FR2993063B1 (fr) * 2012-07-05 2014-08-22 Thales Sa Procede d'aide a la navigation permettant de gerer une contrainte verticale de maniere anticipee
FR2994286B1 (fr) * 2012-08-02 2014-08-22 Airbus Operations Sas Procede et dispositif d'aide a la gestion du vol d'un aeronef
US10013236B2 (en) * 2013-03-06 2018-07-03 The Boeing Company Real-time adaptive speed scheduler
US9047763B2 (en) 2013-03-15 2015-06-02 Honeywell International Inc. Methods and systems for representing time of arrival information on a cockpit display
US9026275B1 (en) * 2013-07-24 2015-05-05 Shih-Yih Young In-flight generation of RTA-compliant optimal profile descent paths
EP2849167B1 (fr) * 2013-09-13 2016-04-27 The Boeing Company Procédé de commande des arrivées d'avion à un point de cheminement
FR3016975B1 (fr) * 2014-01-24 2016-01-15 Thales Sa Procede d'aide a la navigation pour la tenue de contraintes temporelles multiples
US9625261B2 (en) 2014-09-04 2017-04-18 Honeywell International Inc. System and method for managing speed constraints during required time of arrival operations
CN107850439A (zh) * 2015-06-04 2018-03-27 山德尔埃维翁尼克斯有限公司 垂直飞行显示器的系统和方法
ES2707449T3 (es) 2015-06-26 2019-04-03 Boeing Co Método y sistema para controlar el vuelo de una aeronave sometida a al menos dos tiempos requeridos de restricciones de llegada
EP3109724B1 (fr) 2015-06-26 2022-02-09 The Boeing Company Procédé et système de commande de vol d'un avion soumis à une contrainte d'heure d'arrivée requise
FR3057986B1 (fr) * 2016-10-20 2021-04-30 Thales Sa Procede et systeme de determination d'un profil de descente et de rejointe synchrone en poussee minimale pour un aeronef
US10388170B2 (en) * 2017-08-14 2019-08-20 Honeywell International Inc. Speed-constrained flight management methods and systems
US10777085B2 (en) 2018-04-05 2020-09-15 GE Aviation Sytems LLC Efficient flight profiles with multiple RTA constraints
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

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5121325A (en) * 1990-04-04 1992-06-09 Smiths Industries Aerospace & Defense Systems, Inc. Required time of arrival (RTA) control system
US7664601B2 (en) * 1999-11-10 2010-02-16 Honeywell International Inc. Weather incident prediction
US6507782B1 (en) * 2001-05-14 2003-01-14 Honeywell International Inc. Aircraft control system for reaching a waypoint at a required time of arrival
US6600991B1 (en) * 2001-08-14 2003-07-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Neighboring optimal aircraft guidance in a general wind environment
JP3742336B2 (ja) * 2001-12-20 2006-02-01 株式会社東芝 航法支援装置、この航法支援装置を搭載する航空機、航法支援方法、および航法支援処理プログラム
EP1770365B1 (fr) * 2005-09-30 2011-11-16 Saab Ab Procédé de planification de la vitesse d'un véhicule le long d'une route
FR2894046B1 (fr) * 2005-11-28 2008-02-15 Airbus France Sas Procede de detection d'une erreur d'entree d'un des parametres de decollage dans un systeme de management de vol
US20070150123A1 (en) * 2005-12-08 2007-06-28 The Boeing Company System and method for controlling the airspeed of an aircraft
FR2907952B1 (fr) * 2006-10-26 2008-12-19 Airbus France Sa Procede et dispositif d'aide au guidage d'un aeronef le long d'une trajectoire de vol.
FR2913780B1 (fr) * 2007-03-13 2014-07-18 Airbus France Procede et dispositif d'aide au guidage d'un aeronef
FR2923032B1 (fr) * 2007-10-31 2010-11-12 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef en vue d'une phase de descente.
FR2930053B1 (fr) * 2008-04-14 2013-09-20 Airbus France Procede et dispositif de guidage d'un aeronef
US8010267B2 (en) * 2008-10-31 2011-08-30 General Electric Company Methods and system for time of arrival control using available speed authority
FR2938327B1 (fr) * 2008-11-07 2010-12-10 Thales Sa Procede pour la determination de la vitesse d'un aeronef
FR2938682B1 (fr) * 2008-11-14 2013-03-22 Airbus France Procede et dispositif d'asservissement en vitesse d'un aeronef lors d'une phase d'approche
US8150588B2 (en) * 2008-11-25 2012-04-03 General Electric Company Methods and system for time of arrival control using time of arrival uncertainty
FR2942328B1 (fr) * 2009-02-17 2011-02-25 Thales Sa Procede d'aide a l'elaboration de la strategie de vitesse d'un aeronef en vue de tenir une contrainte de temps

Also Published As

Publication number Publication date
US20110137493A1 (en) 2011-06-09
FR2946161A1 (fr) 2010-12-03
US8332145B2 (en) 2012-12-11

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