DE60227332D1 - Verfahren und Vorrichtung zur Steuerungshilfe in einem Flugzeug - Google Patents

Verfahren und Vorrichtung zur Steuerungshilfe in einem Flugzeug

Info

Publication number
DE60227332D1
DE60227332D1 DE60227332T DE60227332T DE60227332D1 DE 60227332 D1 DE60227332 D1 DE 60227332D1 DE 60227332 T DE60227332 T DE 60227332T DE 60227332 T DE60227332 T DE 60227332T DE 60227332 D1 DE60227332 D1 DE 60227332D1
Authority
DE
Germany
Prior art keywords
aircraft
symbol
maneuver
margin
diving
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.)
Expired - Lifetime
Application number
DE60227332T
Other languages
English (en)
Inventor
Eric Godard
David Chabe
Jacques Espinasse
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
Original Assignee
Airbus Operations SAS
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 Operations SAS filed Critical Airbus Operations SAS
Application granted granted Critical
Publication of DE60227332D1 publication Critical patent/DE60227332D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00Arrangements or adaptations of instruments
    • 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
    • G01C23/005Flight directors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Traffic Control Systems (AREA)
  • Indication In Cameras, And Counting Of Exposures (AREA)
DE60227332T 2001-11-08 2002-09-26 Verfahren und Vorrichtung zur Steuerungshilfe in einem Flugzeug Expired - Lifetime DE60227332D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0114451A FR2831871B1 (fr) 2001-11-08 2001-11-08 Procede et dispositif d'aide au pilotage d'un aeronef

Publications (1)

Publication Number Publication Date
DE60227332D1 true DE60227332D1 (de) 2008-08-14

Family

ID=8869183

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60227332T Expired - Lifetime DE60227332D1 (de) 2001-11-08 2002-09-26 Verfahren und Vorrichtung zur Steuerungshilfe in einem Flugzeug

Country Status (7)

Country Link
US (3) US6937166B2 (de)
EP (1) EP1310769B1 (de)
AT (1) ATE399979T1 (de)
CA (1) CA2406334C (de)
DE (1) DE60227332D1 (de)
FR (1) FR2831871B1 (de)
RU (1) RU2241642C2 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
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FR2870514B1 (fr) * 2004-05-18 2006-07-28 Airbus France Sas Indicateur de pilotage determinant la pente maximale pour le pilotage d'un aeronef en suivi de terrain
FR2912502B1 (fr) * 2007-02-13 2009-03-27 Thales Sa Procede de traitement temps reel de donnees topographiques dans un aeronef,en vue de leur affichage
FR2916541B1 (fr) * 2007-05-25 2014-11-21 Thales Sa Dispositif de visualisation tete haute pour aeronef comprenant des moyens d'affichage d'une symbologie dediee a l'evitement d'obstacles.
US8188889B2 (en) * 2007-12-14 2012-05-29 The Boeing Company Method and system for display of traffic information in the flight deck
US8041504B2 (en) 2007-12-17 2011-10-18 The Boeing Company Method and system for display of guidance reference for traffic situational awareness
RU2455201C1 (ru) * 2010-10-28 2012-07-10 Открытое акционерное общество "Российская самолетостроительная корпорация "МиГ" Способ управления самолетом с учетом стабилизации заданной скорости полета
ES2694427T3 (es) * 2013-06-06 2018-12-20 The Boeing Company Método y sistema de control de velocidad de la aeronave
US9529010B2 (en) * 2013-06-17 2016-12-27 Honeywell International Inc. Flight deck display systems and methods for visually indicating low speed change conditions during takeoff and landing
US9983023B2 (en) * 2015-04-07 2018-05-29 Aspen Avionics, Inc. System and method for angle of attack indication with no dedicated sensors and aircraft information
FR3037413B1 (fr) * 2015-06-11 2017-07-21 Thales Sa Dispositif electronique et procede d'aide au pilotage d'un aeronef, avec calcul et affichage d'au moins une marge en roulis, produit programme d'ordinateur associe
CN111060709B (zh) * 2019-12-06 2021-10-15 江西洪都航空工业集团有限责任公司 一种无人机人在环平显显示用速度矢量指示符驱动方法

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FR2521520A1 (fr) * 1982-02-15 1983-08-19 Daude Martine Ailettes marginales a angles d'attaque variables
US4590475A (en) * 1983-10-24 1986-05-20 The United States Of America As Represented By The Secretary Of The Army Stall avoidance system for aircraft
US4910513A (en) * 1985-11-20 1990-03-20 The Boeing Company Apparatus and methods for generating a stall warning margin on an aircraft attitude indicator display
US4764872A (en) * 1986-07-16 1988-08-16 Honeywell Inc. Vertical flight path and airspeed control system for aircraft
US4924401A (en) * 1987-10-30 1990-05-08 The United States Of America As Represented By The Secretary Of The Air Force Aircraft ground collision avoidance and autorecovery systems device
US5003305A (en) * 1988-10-24 1991-03-26 The Boeing Company Apparatus and method for displaying aircraft flight path angle on an attitude display indicator
FR2666428B1 (fr) * 1990-09-05 1994-09-23 Aerospatiale Procede de visualisation sur un ecran a bord d'un avion, de symboles d'aide au pilotage.
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
US5248968A (en) * 1991-12-06 1993-09-28 The Boeing Company Tcas ii pitch guidance control law and display symbol
US5595357A (en) * 1994-07-05 1997-01-21 The B. F. Goodrich Company Aircraft stall warning system
FR2725803B1 (fr) * 1994-10-18 1997-01-03 Sextant Avionique Dispositif optoelectronique d'assistance au pilotage d'un aeronef
DE69625835T2 (de) 1995-03-02 2003-11-13 Thales Avionics Sa Steueranordnung eines handgesteuerten Flugzeugsystemes mit insbesondere einem Head-Up-Display
FR2733061B1 (fr) * 1995-04-13 1997-05-23 Sextant Avionique Dispositif optoelectronique d'aide au pilotage d'un aeronef par mauvaise visibilite
US5978715A (en) * 1997-10-15 1999-11-02 Dassault Aviation Apparatus and method for aircraft display and control
US5912627A (en) * 1997-10-17 1999-06-15 Alexander; William J. Device and method for indicating if an airplane is operating within operating limits
US6271769B1 (en) * 1997-12-02 2001-08-07 Proprietary Software Systems, Inc. Apparatus and method for measuring and displaying angular deviations from angle of zero lift for air vehicles
US6062513A (en) * 1998-09-14 2000-05-16 The Boeing Company Total energy based flight control system
US6169496B1 (en) * 1998-12-09 2001-01-02 Exigent International, Inc. Banked flight stall warning device and method
US6246929B1 (en) * 1999-06-16 2001-06-12 Lockheed Martin Corporation Enhanced stall and recovery control system

Also Published As

Publication number Publication date
EP1310769A1 (de) 2003-05-14
ATE399979T1 (de) 2008-07-15
FR2831871B1 (fr) 2004-08-13
CA2406334A1 (fr) 2003-05-08
US7015829B2 (en) 2006-03-21
US20030137434A1 (en) 2003-07-24
FR2831871A1 (fr) 2003-05-09
US20040155798A1 (en) 2004-08-12
US6980128B2 (en) 2005-12-27
US20040155799A1 (en) 2004-08-12
CA2406334C (fr) 2009-07-28
US6937166B2 (en) 2005-08-30
EP1310769B1 (de) 2008-07-02
RU2241642C2 (ru) 2004-12-10

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