FR2847553B1 - Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segment - Google Patents
Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segmentInfo
- Publication number
- FR2847553B1 FR2847553B1 FR0214872A FR0214872A FR2847553B1 FR 2847553 B1 FR2847553 B1 FR 2847553B1 FR 0214872 A FR0214872 A FR 0214872A FR 0214872 A FR0214872 A FR 0214872A FR 2847553 B1 FR2847553 B1 FR 2847553B1
- Authority
- FR
- France
- Prior art keywords
- interception
- assisting
- segment
- aircraft
- tracking
- 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
Links
Classifications
-
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/02—Control of position or course in two dimensions
- G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0214872A FR2847553B1 (fr) | 2002-11-27 | 2002-11-27 | Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segment |
US10/723,064 US7237747B1 (en) | 2002-11-27 | 2003-11-26 | Device for assisting an airplane in intercepting a segment of a flight path utilizing positional and ground speed indicators |
US11/636,439 US7367526B2 (en) | 2002-11-27 | 2006-12-11 | Device and system for assistance within interception by an aircraft of a flight path segment |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0214872A FR2847553B1 (fr) | 2002-11-27 | 2002-11-27 | Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segment |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2847553A1 FR2847553A1 (fr) | 2004-05-28 |
FR2847553B1 true FR2847553B1 (fr) | 2004-12-31 |
Family
ID=32241666
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0214872A Expired - Lifetime FR2847553B1 (fr) | 2002-11-27 | 2002-11-27 | Dispositif d'aide a l'interception par un aeronef d'un segment d'une trajectoire situee dans un plan horizontal et systeme d'aide a l'interception et au suivi d'un tel segment |
Country Status (2)
Country | Link |
---|---|
US (2) | US7237747B1 (fr) |
FR (1) | FR2847553B1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101203731B (zh) * | 2005-06-21 | 2012-07-18 | 空中客车运营简化股份公司 | 用于按照飞行计划飞行的飞行器的显示方法和设备 |
Families Citing this family (27)
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---|---|---|---|---|
US7091881B2 (en) * | 2003-03-31 | 2006-08-15 | Sikorsky Aircraft Corporation | Integrated hover display with augmented approach to hover symbology cueing for degraded visual environmental conditions |
FR2897712B1 (fr) * | 2006-02-20 | 2008-04-04 | Airbus France Sas | Dispositif d'aide au pilotage d'un aeronef lors d'une phase d'approche en vue d'un atterrissage. |
US8027756B2 (en) * | 2006-12-07 | 2011-09-27 | The Boeing Company | Integrated approach navigation system, method, and computer program product |
US7698026B2 (en) * | 2007-06-14 | 2010-04-13 | The Boeing Company | Automatic strategic offset function |
CA2694177A1 (fr) * | 2007-07-21 | 2009-01-29 | Peter Lyons | Appareil et procede d'indication d'une saturation d'instrument d'ecart de route |
US8996309B2 (en) * | 2007-07-21 | 2015-03-31 | Aspen Avionics, Inc. | Apparatus and method to indicate instrument saturation |
FR2920232B1 (fr) * | 2007-08-22 | 2015-02-27 | Airbus France | Procede et dispositif d'aide au pilotage d'un avion |
FR2928726B1 (fr) * | 2008-03-11 | 2013-05-17 | Thales Sa | Jonction d'une trajectoire civile et d'une trajectoire militaire |
US8155800B2 (en) * | 2008-06-19 | 2012-04-10 | Honeywell International Inc. | System for displaying required navigation performance on a horizontal situation indicator |
US7961115B2 (en) * | 2008-06-19 | 2011-06-14 | Honeywell International Inc. | System for displaying required navigation performance on a horizontal situation indicator |
EP2318278A4 (fr) * | 2008-07-30 | 2013-07-03 | L 3 Comm Avionics Systems Inc | Écrans de vol évolués pour approches de précision et de non-précision |
US9330573B2 (en) | 2009-06-25 | 2016-05-03 | Honeywell International Inc. | Automated decision aid tool for prompting a pilot to request a flight level change |
US8271152B2 (en) * | 2010-03-10 | 2012-09-18 | Honeywell International Inc. | System and method for rendering an onboard aircraft display for use with in-trail procedures |
US8417397B2 (en) | 2010-05-05 | 2013-04-09 | Honeywell International Inc. | Vertical profile display with variable display boundaries |
US9020681B2 (en) | 2010-06-08 | 2015-04-28 | Honeywell International Inc. | Display of navigation limits on an onboard display element of a vehicle |
US9495883B2 (en) * | 2011-08-02 | 2016-11-15 | Honeywell International Inc. | System and method for displaying a procedure to an aircrew member |
EP2573522B1 (fr) * | 2011-09-21 | 2015-01-14 | The Boeing Company | Affichage de guidage de vitesse d'avion |
US8478513B1 (en) | 2012-01-20 | 2013-07-02 | Honeywell International Inc. | System and method for displaying degraded traffic data on an in-trail procedure (ITP) display |
US8554394B2 (en) | 2012-02-28 | 2013-10-08 | Honeywell International Inc. | System and method for rendering an aircraft cockpit display for use with an in-trail procedure (ITP) |
FR2988202B1 (fr) * | 2012-03-13 | 2015-05-15 | Thales Sa | Procede d'aide a la navigation pour le suivi de la performance de navigation en lineaire ou angulaire |
US8781649B2 (en) | 2012-03-19 | 2014-07-15 | Honeywell International Inc. | System and method for displaying in-trail procedure (ITP) opportunities on an aircraft cockpit display |
FR3017703B1 (fr) * | 2014-02-14 | 2017-12-22 | Thales Sa | Procede et systeme de determination de la compatibilite d'un guidage angulaire avec une approche |
EP3304232A4 (fr) * | 2015-06-02 | 2019-01-23 | Sandel Avionics, INC. | Système et procédé pour panneau de guidage de chemin |
FR3044086B1 (fr) | 2015-11-24 | 2018-05-18 | Airbus Helicopters | Procede et dispositif de calcul d'une trajectoire securisee depuis la position courante d'un aeronef jusqu'a un point d'attache |
US10242578B2 (en) * | 2016-08-01 | 2019-03-26 | Ge Aviation Systems Llc | Flight path management system |
US11781875B2 (en) * | 2019-08-21 | 2023-10-10 | Toyota Motor Engineering & Manufacturing North America, Inc. | Apparatus and method for forming and analyzing connected roads |
US20230035682A1 (en) * | 2019-12-17 | 2023-02-02 | Kt Corporation | Method and device for setting drone flight path |
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US2932023A (en) * | 1955-08-04 | 1960-04-05 | Aircraft Radio Corp | Aircraft course director |
US3140391A (en) * | 1959-06-29 | 1964-07-07 | Tasker Instr Corp | Apparatus for ground computed radial navigation |
GB931310A (en) * | 1961-09-19 | 1963-07-17 | Communications Patents Ltd | Improvements in or relating to flight training apparatus |
US3383679A (en) * | 1966-07-15 | 1968-05-14 | Roger P. Baird Jr. | Visual landing simulator for instrument flying |
US3521227A (en) * | 1966-10-10 | 1970-07-21 | Kaiser Aerospace & Electronics | Display system for providing integrated display of aircraft information |
US3520994A (en) * | 1967-01-12 | 1970-07-21 | Kaiser Aerospace & Electronics | Combination raster and calligraphic scanning techniques for aircraft displays |
US3574262A (en) * | 1967-05-25 | 1971-04-13 | Itek Corp | Cinematographic apparatus |
US3573827A (en) * | 1968-04-01 | 1971-04-06 | Bendix Corp | Runway centerline display |
US3697022A (en) * | 1970-07-06 | 1972-10-10 | Sfim | Method and apparatus for aircraft guidance |
US3824381A (en) * | 1972-05-25 | 1974-07-16 | Bendix Corp | Aircraft control system using inertial signals |
US3989209A (en) * | 1974-06-26 | 1976-11-02 | The Bendix Corporation | Apparatus for guiding an aircraft along a multi-segment path when landing the craft |
US4078317A (en) * | 1976-07-30 | 1978-03-14 | Wheatley Ronald B | Flight simulator system |
US4368517A (en) * | 1978-03-16 | 1983-01-11 | Bunker Ramo Corporation | Aircraft landing display system |
US4354240A (en) * | 1980-03-24 | 1982-10-12 | Sperry Corporation | Flight path transition control apparatus with predictive roll command |
US4384338A (en) * | 1980-12-24 | 1983-05-17 | The Singer Company | Methods and apparatus for blending computer image generated features |
US4533999A (en) * | 1981-08-19 | 1985-08-06 | The Boeing Company | Aircraft roll steering command system |
US5308022A (en) * | 1982-04-30 | 1994-05-03 | Cubic Corporation | Method of generating a dynamic display of an aircraft from the viewpoint of a pseudo chase aircraft |
US4972321A (en) * | 1989-04-24 | 1990-11-20 | Honeywell Inc. | Lateral axis rollout control for aircraft |
US5023796A (en) * | 1989-10-03 | 1991-06-11 | Honeywell, Inc. | Flight control apparatus with predictive heading/track hold command |
US5371581A (en) * | 1993-03-08 | 1994-12-06 | Schwartz Electro-Optics, Inc. | Helicopter obstacle warning system |
US5465142A (en) * | 1993-04-30 | 1995-11-07 | Northrop Grumman Corporation | Obstacle avoidance system for helicopters and other aircraft |
FR2725691B1 (fr) * | 1994-10-18 | 1997-01-03 | Sextant Avionique | Dispositif d'aide au pilotage, en phase d'atterrissage, d'un aeronef |
FR2729480B1 (fr) * | 1995-01-16 | 1997-04-04 | Sextant Avionique | Procede de pilotage d'un aerodyne par asservissement sur une trajectoire horizontale determinee a partir de points de passage |
US5797106A (en) * | 1996-03-29 | 1998-08-18 | The Boeing Company | Method and apparatus for an improved flight management system providing for linking of an outbound course line from a predetermined position with an existing flight plan |
FR2752051B1 (fr) * | 1996-08-02 | 1998-10-30 | Sextant Avionique | Dispositif d'assistance au guidage d'un vehicule sur une trajectoire |
US5995901A (en) * | 1996-09-30 | 1999-11-30 | Rockwell International Corporation | Automatic view adjusting flight plan display |
FR2764863B1 (fr) * | 1997-06-23 | 1999-08-20 | Eurocopter France | Indicateur de position pour aeronef |
US5978715A (en) * | 1997-10-15 | 1999-11-02 | Dassault Aviation | Apparatus and method for aircraft display and control |
US6501392B2 (en) * | 1998-02-09 | 2002-12-31 | Honeywell International Inc. | Aircraft weather information system |
FR2783500B1 (fr) * | 1998-09-23 | 2000-12-08 | Eurocopter France | Dispositif d'aide au pilotage d'un aeronef, notamment a voilure tournante et en particulier un helicoptere |
EP1091190A3 (fr) * | 1999-09-14 | 2001-08-16 | Honeywell Inc. | Méthodes et dispositifs de projection et de rendu de données organisées de façon géospatiale |
US6664989B1 (en) * | 1999-10-18 | 2003-12-16 | Honeywell International Inc. | Methods and apparatus for graphical display interaction |
FR2801967B1 (fr) * | 1999-12-07 | 2002-04-12 | Eurocopter France | Indicateur de variable pour aeronef |
FR2803655B1 (fr) * | 2000-01-07 | 2002-06-14 | Thomson Csf Sextant | Calculateur de vol lissant la trajectoire d'un aeronef sur plusieurs sequences |
US6347633B1 (en) | 2000-01-14 | 2002-02-19 | First Circle Medical, Inc. | Treatment of hepatitis C using hyperthermia |
JP3943797B2 (ja) * | 2000-03-31 | 2007-07-11 | キヤノン株式会社 | 画像形成装置 |
DE10027863C2 (de) * | 2000-06-06 | 2003-07-03 | Eads Deutschland Gmbh | Bahnregler für Fahrzeuge mit einer von einer Anströmung beeinflußten Bahn |
US6980198B1 (en) * | 2000-09-19 | 2005-12-27 | Honeywell International Inc. | Multifunction keyboard for advanced cursor driven avionic flight decks |
US6700482B2 (en) * | 2000-09-29 | 2004-03-02 | Honeywell International Inc. | Alerting and notification system |
US6571155B2 (en) * | 2001-07-02 | 2003-05-27 | The Boeing Company | Assembly, computer program product and method for displaying navigation performance based flight path deviation information |
US6870490B2 (en) * | 2001-08-23 | 2005-03-22 | Honeywell International Inc. | Display of altitude and path capture trajectories |
US6625537B2 (en) * | 2002-01-23 | 2003-09-23 | Honeywell | Methods and apparatus for assembling a flight plan |
SE523828C2 (sv) * | 2002-02-08 | 2004-05-25 | Saab Ab | Metod och system för att beräkna en flygrutt |
US6985801B1 (en) * | 2002-02-28 | 2006-01-10 | Garmin International, Inc. | Cockpit instrument panel systems and methods with redundant flight data display |
US6678588B2 (en) * | 2002-04-12 | 2004-01-13 | Honeywell International Inc. | Terrain augmented 3D flight path display for flight management systems |
US6744382B1 (en) * | 2002-04-19 | 2004-06-01 | Rockwell Collins | Method and apparatus for guiding an aircraft through a cluster of hazardous areas |
US6905091B2 (en) * | 2003-07-14 | 2005-06-14 | Supersonic Aerospace International, Llc | System and method for controlling the acoustic signature of a device |
CN101030948A (zh) | 2006-03-02 | 2007-09-05 | 华为技术有限公司 | 一种基于ip的消息路由方法和系统 |
-
2002
- 2002-11-27 FR FR0214872A patent/FR2847553B1/fr not_active Expired - Lifetime
-
2003
- 2003-11-26 US US10/723,064 patent/US7237747B1/en not_active Expired - Fee Related
-
2006
- 2006-12-11 US US11/636,439 patent/US7367526B2/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101203731B (zh) * | 2005-06-21 | 2012-07-18 | 空中客车运营简化股份公司 | 用于按照飞行计划飞行的飞行器的显示方法和设备 |
Also Published As
Publication number | Publication date |
---|---|
US20070145183A1 (en) | 2007-06-28 |
US7237747B1 (en) | 2007-07-03 |
US7367526B2 (en) | 2008-05-06 |
US20070145184A1 (en) | 2007-06-28 |
FR2847553A1 (fr) | 2004-05-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name |
Owner name: AIRBUS HELICOPTERS, FR Effective date: 20140602 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
PLFP | Fee payment |
Year of fee payment: 16 |