BR0201166A - Processo e dispositivo de assistência à pilotagem de uma aeronave - Google Patents

Processo e dispositivo de assistência à pilotagem de uma aeronave

Info

Publication number
BR0201166A
BR0201166A BR0201166-2A BR0201166A BR0201166A BR 0201166 A BR0201166 A BR 0201166A BR 0201166 A BR0201166 A BR 0201166A BR 0201166 A BR0201166 A BR 0201166A
Authority
BR
Brazil
Prior art keywords
aircraft
trace
data
altitude
graduated
Prior art date
Application number
BR0201166-2A
Other languages
English (en)
Inventor
Benoit Morizet
Jean-Sebastien Vial
Original Assignee
Airbus France
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 France filed Critical Airbus France
Publication of BR0201166A publication Critical patent/BR0201166A/pt

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00Combined 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Radio Relay Systems (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Tires In General (AREA)

Abstract

"PROCESSO E DISPOSITIVO DE ASSISTêNCIA à PILOTAGEM DE UMA AERONAVE". O processo prevê que se apresente numa tela de visualização (5), uma apresentação de informações (IF1) que representa, pelo menos, um plano vertical ao longo de uma trajetória de vóo teórica da aeronave e que comporta um sistema de eixos (8, 9), do qual um eixo de ordenada (8) é graduado em altitude, e um eixo de abscissa (9) é graduado em distância a partir da posição da aeronave, um símbolo particular (7) representando a aeronave, o qual se encontra sobre o eixo de ordenada (8) numa posição representativa da altitude da dita aeronave, e um primeiro traçado (T1) representando uma trajetória de vóo teórica da dita aeronave no plano vertical. A dita apresentação de informações (IF1) comporta, além disso, um segundo traçado (T2) correspondendo a uma altitude de segurança, e um terceiro traçado (T3) correspondendo a um contorno do terreno (10) no plano vertical.
BR0201166-2A 2001-03-27 2002-03-25 Processo e dispositivo de assistência à pilotagem de uma aeronave BR0201166A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0104083A FR2822944B1 (fr) 2001-03-27 2001-03-27 Procede et dispositif d'assistance au pilotage d'un aeronef, notamment d'un avion de transport

Publications (1)

Publication Number Publication Date
BR0201166A true BR0201166A (pt) 2003-06-10

Family

ID=8861568

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0201166-2A BR0201166A (pt) 2001-03-27 2002-03-25 Processo e dispositivo de assistência à pilotagem de uma aeronave

Country Status (7)

Country Link
US (1) US6505102B2 (pt)
EP (1) EP1245929B1 (pt)
AT (1) ATE449954T1 (pt)
BR (1) BR0201166A (pt)
CA (1) CA2374174C (pt)
DE (1) DE60234482D1 (pt)
FR (1) FR2822944B1 (pt)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6964672B2 (en) * 1999-05-07 2005-11-15 Salviac Limited Support frame for an embolic protection device
US6995690B1 (en) * 1999-07-30 2006-02-07 The Boeing Company Vertical situation display terrain/waypoint swath, range to target speed, and blended airplane reference
US6593858B2 (en) * 2001-09-12 2003-07-15 Honeywell International Inc. Methods and apparatus for generating a vertical situational image of a vehicle
FR2847700B1 (fr) * 2002-11-22 2005-01-14 Thales Sa Procede de synthese d'une image d'intervisibilite tridimensionnelle
FR2852683B1 (fr) * 2003-03-19 2005-05-20 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche de non precision pendant une phase d'atterrissage.
US6934608B2 (en) * 2003-07-09 2005-08-23 Honeywell International Inc. Integrated vertical situation display
FR2870519B1 (fr) * 2004-05-18 2006-08-11 Airbus France Sas Procede et dispositif de guidage d'un aeronef a l'atterrissage
FR2870604B1 (fr) * 2004-05-18 2006-08-11 Airbus France Sas Procede et dispositif de securisation d'un vol a basse altitude d'un aeronef
US7783393B2 (en) * 2004-06-30 2010-08-24 The Boeing Company Enhanced vertical situation display
FR2874258B1 (fr) * 2004-08-10 2006-11-03 Thales Sa Procede d'affichage d'informations cartographiques et de zones aeronautiques sur ecran d'aeronef
FR2875916B1 (fr) * 2004-09-28 2015-06-26 Eurocopter France Procede et dispositif d'aide au pilotage d'un aeronef a voilure tournante au voisinage d'un point de pose ou de decollage
US7477164B1 (en) * 2004-12-08 2009-01-13 Rockwell Collins, Inc. Vertical profile display using color filled bands to provide terrain awareness
US7389163B1 (en) * 2005-02-17 2008-06-17 The Boeing Company Procedure to minimize the risk of air collision for personal mid-air vehicles
FR2894356B1 (fr) * 2005-12-07 2008-01-18 Thales Sa Procede de synthese d'images d'intervisibilte
FR2895793B1 (fr) 2006-01-05 2008-02-01 Airbus France Sas Procede et dispositif d'assistance au pilotage d'un aeronef.
FR2895794B1 (fr) * 2006-01-05 2008-02-15 Airbus France Sas Procede et dispositif d'assistance au pilotage d'un aeronef en vol libre.
WO2009035757A2 (en) * 2007-07-11 2009-03-19 Sandel Avionics, Inc. Flight management system having interactive flight plan selection arrangement
FR2923008B1 (fr) * 2007-10-26 2010-01-08 Thales Sa Procede et dispositif d'affichage de previsions sur un plan de navigation
US8032268B2 (en) * 2008-09-29 2011-10-04 Honeywell International Inc. Methods and systems for indicating whether an aircraft is below a minimum altitude criterion for a sector
US20100131126A1 (en) 2008-11-21 2010-05-27 Honeywell International Inc. System and display element for displaying waypoint markers with integrated altitude constraint information
FR2944596B1 (fr) * 2009-04-21 2011-06-03 Thales Sa Dispositif de visualisation pour aeronef comprenant des moyens d'affichage des tendances d'evolution meteorologique
FR2946780B1 (fr) * 2009-06-12 2011-07-15 Thales Sa Procede et dispositif d'affichage des limites de marges de vol pour un aeronef
FR2956499B1 (fr) * 2010-02-15 2012-04-13 Airbus Operations Sas Procede et dispositif permettant l'exploitation fonctionnelle, dans un aeronef, d'un grand nombre d'informations issues de differentes sources
US9053630B2 (en) * 2010-02-17 2015-06-09 The Boeing Company Methods and systems for depicting a data driven minimum safe altitude
US8412392B2 (en) * 2010-02-24 2013-04-02 Honeywell International Inc. Methods and systems for displaying predicted downpath parameters in a vertical profile display
US8374776B2 (en) * 2010-03-31 2013-02-12 The Boeing Company Methods and apparatus for indicating a relative altitude in one or more directions
US9020681B2 (en) 2010-06-08 2015-04-28 Honeywell International Inc. Display of navigation limits on an onboard display element of a vehicle
US8970402B1 (en) * 2012-02-23 2015-03-03 Rockwell Collins, Inc. System, device, and method for varying the visibility of symbols depicted in a vertical situation display
US8798815B1 (en) 2013-03-13 2014-08-05 Honeywell International Inc. System and method alerting an aircrew of threshold altitudes
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.
US8972082B2 (en) * 2013-07-25 2015-03-03 Honeywell International Inc. Aircraft flight deck displays and systems and methods for displaying integrated minimum safe altitude and minimum vectoring altitude information on a display device in an aircraft
DE102014116448A1 (de) * 2014-11-11 2016-05-12 Infineon Technologies Ag Verfahren und Vorrichtung zur Verarbeitung von Radarsignalen
US9646503B2 (en) * 2015-02-11 2017-05-09 Honeywell International Inc. Cockpit display systems and methods for generating navigation displays including landing diversion symbology
WO2016149039A1 (en) * 2015-03-17 2016-09-22 Sikorsky Aircraft Corporation Trajectory control of a vehicle
FR3035962B1 (fr) 2015-05-04 2017-04-21 Airbus Operations Sas Procede, dispositif et systeme d'affichage d'un profil vertical de vol d'un aeronef
FR3036511B1 (fr) * 2015-05-19 2019-12-20 Dassault Aviation Systeme de visualisation d'informations relatives a un vol d'un aeronef et procede associe
US9536435B1 (en) 2015-07-13 2017-01-03 Double Black Aviation Technology L.L.C. System and method for optimizing an aircraft trajectory
CN109993996A (zh) * 2018-01-02 2019-07-09 上海航空电器有限公司 一种直升机地形提示与告警系统的显示方法
FR3078848B1 (fr) * 2018-03-06 2021-04-09 Thales Sa Terminal d'operateur d'un systeme avionique de pilotage d'un aeronef
FR3099263B1 (fr) * 2019-07-22 2021-12-17 Thales Sa Procede et dispositif electronique de gestion de l'affichage d'une cartographie terrain pour un aeronef, programme d'ordinateur et systeme d'affichage associes

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4373184A (en) * 1979-12-26 1983-02-08 The Boeing Company Vertical flight path steering system for aircraft
FR2689231B1 (fr) * 1992-03-26 1996-09-27 Aerospatiale Ste Nat Indle Procede et dispositif d'assistance au pilotage d'un aerodyne par la representation graphique du plan de vol vertical de cet aerodyne
FR2744525B1 (fr) * 1996-02-02 1998-03-06 Sextant Avionique Procede et dispositif d'aide a la navigation aerienne
US6057788A (en) * 1997-06-30 2000-05-02 Cummings; Thomas F. Remote control keypad unit
US6112141A (en) * 1997-10-15 2000-08-29 Dassault Aviation Apparatus and method for graphically oriented aircraft display and control
US6336835B1 (en) * 1999-05-25 2002-01-08 Suzuki Kabushiki Kaisha Steering system of outboard motor
CA2376208C (en) * 1999-07-30 2007-04-24 The Boeing Company Vertical situation display terrain/waypoint swath, range to target speed, and blended airplane reference
US6366836B1 (en) * 2000-06-06 2002-04-02 Rockwell Collins, Inc. Method and apparatus for providing adaptive altitude preselector units

Also Published As

Publication number Publication date
CA2374174A1 (fr) 2002-09-27
ATE449954T1 (de) 2009-12-15
FR2822944A1 (fr) 2002-10-04
US20020143439A1 (en) 2002-10-03
DE60234482D1 (de) 2010-01-07
US6505102B2 (en) 2003-01-07
EP1245929B1 (fr) 2009-11-25
EP1245929A2 (fr) 2002-10-02
CA2374174C (fr) 2010-05-25
EP1245929A3 (fr) 2004-06-02
FR2822944B1 (fr) 2003-08-29

Similar Documents

Publication Publication Date Title
BR0201166A (pt) Processo e dispositivo de assistência à pilotagem de uma aeronave
US5745054A (en) Method and apparatus for conformal runway alignment on a head up display
US7218245B2 (en) Head-down aircraft attitude display and method for displaying schematic and terrain data symbology
US5745863A (en) Three dimensional lateral displacement display symbology which is conformal to the earth
ATE146890T1 (de) Vorrichtung zur vorführung einer karte
EP1014104A3 (en) Inertially augmented GPS landing system
EP1273987A3 (en) Assembly, computer program product and method for displaying navigation performance based flight path deviation information
DE3775163D1 (de) Integriertes, redundantes referenzsystem fuer die flugregelung und zur erzeugung von kurs- und lageinformationen.
FR2406831A1 (fr) Systeme de poursuite d'une cible mobile
EP1087210A3 (en) Methods and apparatus for graphical display and editing of flight plans
US20070080828A1 (en) Hybrid centered head-down aircraft attitude display and method for calculating displayed drift angle limit
US8831798B1 (en) Systems and methods for positioning a heading-based image within a track-based image and for generating steering commands to a steerable forward-looking image capture device of an enhanced vision system
ATE181430T1 (de) Vorrichtung zur steuerungshilfe
US2919350A (en) Infrared ranging system
CN109671303A (zh) 用于辅助飞行器着陆的系统和方法
CN104925271B (zh) 升力式飞行器的再入标准轨迹指令的确定方法
JPH08210872A (ja) 航空機の操縦支援用光電子装置
RU119454U1 (ru) Устройство нашлемной системы целеуказания и индикации
JPS56102823A (en) Positioning device
GB1200029A (en) Doppler-inertial navigation system
US6089506A (en) Thermal center flight indicator for gliders
DE602004000072D1 (de) Verfahren und Vorrichtung zur Bestimmung von mindestens einer Angabe bezüglich der vertikalen Position eines Luftfahrzeuges
RU2516857C2 (ru) Способ определения ориентации шлема пилота и устройство нашлемной системы целеуказания и индикации
Milne et al. Maximum likelihood stability and control derivative identification of a Cessna Citation II
JPS57127808A (en) Azimuth and traveling distance finder

Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 12A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2258 DE 15/04/2014.