FR2404200A1 - Collimateur de pilotage d'aeronef - Google Patents
Collimateur de pilotage d'aeronefInfo
- Publication number
- FR2404200A1 FR2404200A1 FR7827239A FR7827239A FR2404200A1 FR 2404200 A1 FR2404200 A1 FR 2404200A1 FR 7827239 A FR7827239 A FR 7827239A FR 7827239 A FR7827239 A FR 7827239A FR 2404200 A1 FR2404200 A1 FR 2404200A1
- Authority
- FR
- France
- Prior art keywords
- piloting
- relates
- flight path
- aircraft pilot
- collimator
- 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.)
- Granted
Links
Classifications
-
- 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
-
- 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
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
- G08G5/21—Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/54—Navigation or guidance aids for approach or landing
-
- 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
- G02B2027/0187—Display position adjusting means not related to the information to be displayed slaved to motion of at least a part of the body of the user, e.g. head, eye
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Optics & Photonics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
L'invention concerne les collimateurs de pilotage. Elle se rapporte à un collimateur de pilotage destiné à présenter une barre de trajectoire de vol, des échelles de tangage et des repères d'arrondi qui sont placés par rapport à la scène extérieure de manière que le pilote, alignant la barre de trajectoire de vol sur la cible voulue, assure le déplacement de l'aéronef suivant une trajectoire d'approche comprenant deux segments d'inclinaisons différentes, avant l'arrondi et la prise de terrain. Application au pilotage des aéronefs lors d'un atterrissage dans une zone urbaine.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/836,012 US4147056A (en) | 1977-09-23 | 1977-09-23 | Multi-segment head-up display for aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2404200A1 true FR2404200A1 (fr) | 1979-04-20 |
FR2404200B1 FR2404200B1 (fr) | 1982-10-22 |
Family
ID=25271012
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7827239A Granted FR2404200A1 (fr) | 1977-09-23 | 1978-09-22 | Collimateur de pilotage d'aeronef |
Country Status (8)
Country | Link |
---|---|
US (1) | US4147056A (fr) |
JP (2) | JPS5544042A (fr) |
CA (1) | CA1103791A (fr) |
DE (1) | DE2838064C2 (fr) |
FR (1) | FR2404200A1 (fr) |
GB (1) | GB2004828B (fr) |
IT (1) | IT1106030B (fr) |
SE (1) | SE443348B (fr) |
Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4368517A (en) * | 1978-03-16 | 1983-01-11 | Bunker Ramo Corporation | Aircraft landing display system |
US4316252A (en) * | 1979-08-10 | 1982-02-16 | The Boeing Company | Apparatus for determining the position of an aircraft with respect to the runway |
FR2487505A1 (fr) * | 1980-07-23 | 1982-01-29 | Dassault Avions | Dispositif d'assistance au pilotage d'un vehicule aerien |
US4554545A (en) * | 1980-10-30 | 1985-11-19 | Mcdonnell Douglas Corporation | Conformal head-up display |
GB2140756B (en) * | 1983-02-10 | 1987-03-18 | Norman Stinson Ritchie | Microprocessor controlled gas turbine aero-engine and navigational system |
FR2580800B1 (fr) * | 1985-04-18 | 1987-07-10 | Dassault Avions | Procede et dispositif pour la representation de l'horizon a bord des aeronefs |
US4740779A (en) * | 1986-04-16 | 1988-04-26 | The Boeing Company | Aircraft panoramic display |
DE3621052A1 (de) * | 1986-06-24 | 1988-01-07 | Aerodata Flugmesstechnik Gmbh | Vorrichtung zur automatischen flugbahnfuehrung von flugzeugen laengs eines leitstrahls |
FR2613502B1 (fr) * | 1987-03-30 | 1989-07-28 | Sfena | Dispositif pour le pilotage d'un aerodyne a partir d'un element de l'environnement exterieur designe par le pilote |
US4843554A (en) * | 1987-08-06 | 1989-06-27 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Airplane takeoff and landing performance monitoring system |
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 |
US4999780A (en) * | 1989-03-03 | 1991-03-12 | The Boeing Company | Automatic reconfiguration of electronic landing display |
SE9103475D0 (sv) * | 1991-11-25 | 1991-11-25 | Polytech Ab | Presentationssystem foer navigering och vaegledning |
US5585813A (en) * | 1992-10-05 | 1996-12-17 | Rockwell International Corporation | All aspect head aiming display |
FR2725803B1 (fr) * | 1994-10-18 | 1997-01-03 | Sextant Avionique | Dispositif optoelectronique d'assistance au pilotage d'un aeronef |
ATE417247T1 (de) | 2002-02-19 | 2008-12-15 | Jeppesen Sanderson Inc | Flughafensrollweg-navigationssystem |
US20040059474A1 (en) * | 2002-09-20 | 2004-03-25 | Boorman Daniel J. | Apparatuses and methods for displaying autoflight information |
US7460029B2 (en) * | 2003-12-24 | 2008-12-02 | The Boeing Company | Systems and methods for presenting and obtaining flight control information |
US7577501B2 (en) | 2004-02-26 | 2009-08-18 | The Boeing Company | Methods and systems for automatically tracking information during flight |
US7751947B2 (en) * | 2004-03-31 | 2010-07-06 | The Boeing Company | Methods and systems for displaying assistance messages to aircraft operators |
US7222017B2 (en) | 2004-06-17 | 2007-05-22 | The Boeing Company | Method and system for entering and displaying ground taxi instructions |
US20060005147A1 (en) * | 2004-06-30 | 2006-01-05 | Hammack Jason L | Methods and systems for controlling the display of maps aboard an aircraft |
US7283064B2 (en) * | 2005-04-12 | 2007-10-16 | Honeywell International, Inc. | System and method for facilitating target aiming and aircraft control using aircraft displays |
US7834779B2 (en) * | 2005-06-29 | 2010-11-16 | Honeywell International Inc. | System and method for increasing visibility of critical flight information on aircraft displays |
US8180562B2 (en) * | 2008-06-04 | 2012-05-15 | The Boeing Company | System and method for taxi route entry parsing |
US8386167B2 (en) * | 2008-11-14 | 2013-02-26 | The Boeing Company | Display of taxi route control point information |
US8344911B1 (en) * | 2010-02-18 | 2013-01-01 | Rockwell Collins, Inc. | System, module, and method for generating non-linearly spaced graduations for a symbolic linear scale |
US8436749B2 (en) | 2010-11-03 | 2013-05-07 | Hamilton Sundstrand Corporation | Failsafe LED control system |
US8831799B1 (en) * | 2013-04-04 | 2014-09-09 | The Boeing Company | Flight director flare guidance |
GB2529684A (en) * | 2014-08-29 | 2016-03-02 | Bae Systems Plc | Image display |
GB2529682A (en) | 2014-08-29 | 2016-03-02 | Bae Systems Plc | Image display |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3851303A (en) * | 1972-11-17 | 1974-11-26 | Sundstrand Data Control | Head up display and pitch generator |
FR2347656A1 (fr) * | 1976-04-05 | 1977-11-04 | Sundstrand Data Control | Collimateur de pilotage |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3128623A (en) * | 1960-09-07 | 1964-04-14 | Sperry Rand Corp | Flight control systems |
US3686626A (en) * | 1970-06-03 | 1972-08-22 | United Control Corp | Aircraft instrument |
US3654806A (en) * | 1970-06-18 | 1972-04-11 | Sundstrand Data Controls Inc | Aircraft instrument |
US3816005A (en) * | 1970-06-22 | 1974-06-11 | Sundstrand Data Control | Head-up display |
FR2170916B1 (fr) * | 1972-02-08 | 1974-12-13 | Thomson Csf |
-
1977
- 1977-09-23 US US05/836,012 patent/US4147056A/en not_active Expired - Lifetime
-
1978
- 1978-08-31 DE DE2838064A patent/DE2838064C2/de not_active Expired
- 1978-09-20 GB GB7837716A patent/GB2004828B/en not_active Expired
- 1978-09-21 SE SE7809920A patent/SE443348B/sv unknown
- 1978-09-22 CA CA311,937A patent/CA1103791A/fr not_active Expired
- 1978-09-22 IT IT51201/78A patent/IT1106030B/it active
- 1978-09-22 FR FR7827239A patent/FR2404200A1/fr active Granted
- 1978-09-22 JP JP11606578A patent/JPS5544042A/ja active Pending
-
1983
- 1983-01-12 JP JP1983001763U patent/JPS58143798U/ja active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3851303A (en) * | 1972-11-17 | 1974-11-26 | Sundstrand Data Control | Head up display and pitch generator |
FR2347656A1 (fr) * | 1976-04-05 | 1977-11-04 | Sundstrand Data Control | Collimateur de pilotage |
Also Published As
Publication number | Publication date |
---|---|
CA1103791A (fr) | 1981-06-23 |
FR2404200B1 (fr) | 1982-10-22 |
IT1106030B (it) | 1985-11-11 |
SE7809920L (sv) | 1979-03-24 |
JPS5544042A (en) | 1980-03-28 |
SE443348B (sv) | 1986-02-24 |
IT7851201A0 (it) | 1978-09-22 |
DE2838064C2 (de) | 1986-10-09 |
GB2004828A (en) | 1979-04-11 |
JPS58143798U (ja) | 1983-09-28 |
US4147056A (en) | 1979-04-03 |
DE2838064A1 (de) | 1979-03-29 |
GB2004828B (en) | 1982-02-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |