FR3056004B1 - Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une manoeuvre d'arrondi. - Google Patents
Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une manoeuvre d'arrondi. Download PDFInfo
- Publication number
- FR3056004B1 FR3056004B1 FR1658590A FR1658590A FR3056004B1 FR 3056004 B1 FR3056004 B1 FR 3056004B1 FR 1658590 A FR1658590 A FR 1658590A FR 1658590 A FR1658590 A FR 1658590A FR 3056004 B1 FR3056004 B1 FR 3056004B1
- Authority
- FR
- France
- Prior art keywords
- load factor
- maneuver
- aircraft
- rounding
- aircraft during
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title abstract 2
- 230000005236 sound signal Effects 0.000 abstract 1
Classifications
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- 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
- 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
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
- G05D1/0016—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement characterised by the operator's input device
-
- 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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0066—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for limitation of acceleration or stress
-
- 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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
- G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Computing Systems (AREA)
- Mathematical Physics (AREA)
- Theoretical Computer Science (AREA)
- Traffic Control Systems (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
Abstract
- Procédé et dispositif d'aide à l'atterrissage d'un aéronef lors d'une manœuvre d'arrondi. - Le dispositif (1) comprend un module d'acquisition (2) pour acquérir des paramètres courants de l'aéronef, un module de calcul (3) pour calculer un facteur de charge courant de l'aéronef, un module de calcul (4) pour calculer un facteur de charge minimum, un module de calcul (5) pour calculer la différence entre le facteur de charge courant et le facteur de charge minimum, et un module d'émission acoustique (6) pour émettre un signal sonore (7) dont le niveau augmente graduellement en fonction du temps lorsque la différence entre le facteur de charge courant et le facteur de charge minimum est inférieure à zéro.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1658590A FR3056004B1 (fr) | 2016-09-14 | 2016-09-14 | Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une manoeuvre d'arrondi. |
US15/689,850 US10274968B2 (en) | 2016-09-14 | 2017-08-29 | Method and device for assisting with the landing of an aircraft during a flare maneuver |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1658590A FR3056004B1 (fr) | 2016-09-14 | 2016-09-14 | Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une manoeuvre d'arrondi. |
FR1658590 | 2016-09-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3056004A1 FR3056004A1 (fr) | 2018-03-16 |
FR3056004B1 true FR3056004B1 (fr) | 2020-12-25 |
Family
ID=57485667
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1658590A Active FR3056004B1 (fr) | 2016-09-14 | 2016-09-14 | Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une manoeuvre d'arrondi. |
Country Status (2)
Country | Link |
---|---|
US (1) | US10274968B2 (fr) |
FR (1) | FR3056004B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3044810A1 (fr) * | 2015-12-04 | 2017-06-09 | Airbus Operations Sas | Systeme d’aide a la gestion du vol d’un aeronef lors d’une phase d’atterrissage. |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2410855A (en) * | 1944-03-15 | 1946-11-12 | Otto C Koppen | Spoiler control means for airplanes |
US3659810A (en) * | 1968-05-20 | 1972-05-02 | James L Robertson | Inherently stable tapered wing flaperon airplane |
US4619110A (en) * | 1983-07-13 | 1986-10-28 | Moore M Samuel | Helicopter engine warning or control system |
GB9003653D0 (en) * | 1990-02-17 | 1990-04-11 | Smiths Industries Plc | Aircraft performance monitoring |
US5722620A (en) * | 1995-05-15 | 1998-03-03 | The Boeing Company | Aircraft pitch-axis stability and command augmentation |
US6671588B2 (en) * | 2001-12-27 | 2003-12-30 | Toyota Jidosha Kabushiki Kaisha | System and method for controlling traveling direction of aircraft |
US6834829B2 (en) * | 2003-01-02 | 2004-12-28 | Percy E. Dunagin, Jr. | Vertical lift aircraft having an enclosed rotary wing |
US8831799B1 (en) | 2013-04-04 | 2014-09-09 | The Boeing Company | Flight director flare guidance |
FR3032044B1 (fr) * | 2015-01-28 | 2020-07-17 | Airbus | Procede et dispositif d'aide a l'atterrissage d'un aeronef lors d'une phase d'arrondi. |
US10150558B2 (en) * | 2016-06-30 | 2018-12-11 | DZYNE Technologies Incorporated | Tilting landing gear systems and methods |
-
2016
- 2016-09-14 FR FR1658590A patent/FR3056004B1/fr active Active
-
2017
- 2017-08-29 US US15/689,850 patent/US10274968B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3056004A1 (fr) | 2018-03-16 |
US20180074515A1 (en) | 2018-03-15 |
US10274968B2 (en) | 2019-04-30 |
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