ATE399979T1 - Verfahren und vorrichtung zur steuerungshilfe in einem flugzeug - Google Patents

Verfahren und vorrichtung zur steuerungshilfe in einem flugzeug

Info

Publication number
ATE399979T1
ATE399979T1 AT02292377T AT02292377T ATE399979T1 AT E399979 T1 ATE399979 T1 AT E399979T1 AT 02292377 T AT02292377 T AT 02292377T AT 02292377 T AT02292377 T AT 02292377T AT E399979 T1 ATE399979 T1 AT E399979T1
Authority
AT
Austria
Prior art keywords
symbol
maneuver
margin
diving
displayed
Prior art date
Application number
AT02292377T
Other languages
German (de)
English (en)
Inventor
Eric Godard
David Chabe
Jacques Espinasse
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
Application granted granted Critical
Publication of ATE399979T1 publication Critical patent/ATE399979T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • 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
    • G01C23/005—Flight directors
AT02292377T 2001-11-08 2002-09-26 Verfahren und vorrichtung zur steuerungshilfe in einem flugzeug ATE399979T1 (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
ATE399979T1 true ATE399979T1 (de) 2008-07-15

Family

ID=8869183

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02292377T ATE399979T1 (de) 2001-11-08 2002-09-26 Verfahren und vorrichtung zur steuerungshilfe in einem flugzeug

Country Status (7)

Country Link
US (3) US6937166B2 (US20040155798A1-20040812-M00009.png)
EP (1) EP1310769B1 (US20040155798A1-20040812-M00009.png)
AT (1) ATE399979T1 (US20040155798A1-20040812-M00009.png)
CA (1) CA2406334C (US20040155798A1-20040812-M00009.png)
DE (1) DE60227332D1 (US20040155798A1-20040812-M00009.png)
FR (1) FR2831871B1 (US20040155798A1-20040812-M00009.png)
RU (1) RU2241642C2 (US20040155798A1-20040812-M00009.png)

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* 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
EP2811359B1 (en) * 2013-06-06 2018-08-08 The Boeing Company Method and system for aircraft speed control
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
CN107980031B (zh) * 2015-04-07 2021-08-24 阿斯潘航空电子有限公司 用于无专用传感器和飞行器信息的迎角指示的系统和方法
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
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Also Published As

Publication number Publication date
CA2406334A1 (fr) 2003-05-08
US20030137434A1 (en) 2003-07-24
EP1310769A1 (fr) 2003-05-14
FR2831871A1 (fr) 2003-05-09
RU2241642C2 (ru) 2004-12-10
US6980128B2 (en) 2005-12-27
CA2406334C (fr) 2009-07-28
US7015829B2 (en) 2006-03-21
US20040155798A1 (en) 2004-08-12
US6937166B2 (en) 2005-08-30
FR2831871B1 (fr) 2004-08-13
EP1310769B1 (fr) 2008-07-02
DE60227332D1 (de) 2008-08-14
US20040155799A1 (en) 2004-08-12

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