ATE339716T1 - Verfahren zur sicherung eines horizontal mit niedriggeschwindigkeit fliegenden flugzeuges - Google Patents
Verfahren zur sicherung eines horizontal mit niedriggeschwindigkeit fliegenden flugzeugesInfo
- Publication number
- ATE339716T1 ATE339716T1 AT05290577T AT05290577T ATE339716T1 AT E339716 T1 ATE339716 T1 AT E339716T1 AT 05290577 T AT05290577 T AT 05290577T AT 05290577 T AT05290577 T AT 05290577T AT E339716 T1 ATE339716 T1 AT E339716T1
- Authority
- AT
- Austria
- Prior art keywords
- aircraft
- securing
- low speed
- aircraft flying
- flying horizontally
- Prior art date
Links
Classifications
-
- 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
- G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
- G05D1/0623—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the pitch
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Radar Systems Or Details Thereof (AREA)
- Vehicle Body Suspensions (AREA)
- Toys (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Seal Device For Vehicle (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0403762A FR2868852B1 (fr) | 2004-04-09 | 2004-04-09 | Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE339716T1 true ATE339716T1 (de) | 2006-10-15 |
Family
ID=34896737
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT05290577T ATE339716T1 (de) | 2004-04-09 | 2005-03-16 | Verfahren zur sicherung eines horizontal mit niedriggeschwindigkeit fliegenden flugzeuges |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US7422176B2 (de) |
| EP (1) | EP1585001B1 (de) |
| AT (1) | ATE339716T1 (de) |
| CA (1) | CA2500841C (de) |
| DE (1) | DE602005000123T2 (de) |
| ES (1) | ES2273320T3 (de) |
| FR (1) | FR2868852B1 (de) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2885706B1 (fr) * | 2005-05-10 | 2007-06-15 | Airbus France Sas | Procede d'aide au decollage d'un aeronef. |
| FR2889342B1 (fr) * | 2005-07-26 | 2010-11-19 | Airbus France | Procede et dispositif de detection d'un risque de collision d'un aeronef avec le terrain environnant |
| AU2006272497B2 (en) | 2005-07-27 | 2012-07-19 | University Of Florida Research Foundation, Inc. | Small compounds that correct protein misfolding and uses thereof |
| US10228692B2 (en) | 2017-03-27 | 2019-03-12 | Gulfstream Aerospace Corporation | Aircraft flight envelope protection and recovery autopilot |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5031102A (en) * | 1979-12-03 | 1991-07-09 | The Boeing Company | Method and apparatus for aircraft pitch and thrust axes control |
| 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 |
| US4764872A (en) * | 1986-07-16 | 1988-08-16 | Honeywell Inc. | Vertical flight path and airspeed control system for aircraft |
| FR2624964B1 (fr) * | 1987-12-22 | 1990-06-01 | Aerospatiale | Systeme de reference de vitesse pour le pilotage d'un aeronef |
| US5079711A (en) * | 1990-02-26 | 1992-01-07 | The Boeing Company | Aircraft high altitude vertical flight path and speed control system |
| FR2688077B1 (fr) * | 1992-02-28 | 1994-05-27 | Aerospatiale | Procede de pilotage d'un avion en mode "maintien de vitesse par action sur la gouverne de profondeur". |
| US5746392A (en) * | 1995-05-15 | 1998-05-05 | The Boeing Company | Autopilot/flight director underspeed protection system |
| FR2747204B1 (fr) * | 1996-04-05 | 1998-06-12 | Aerospatiale | Dispositif pour maintenir la vitesse d'un aeronef a l'interieur d'un domaine de vitesses determine |
-
2004
- 2004-04-09 FR FR0403762A patent/FR2868852B1/fr not_active Expired - Fee Related
-
2005
- 2005-03-16 EP EP05290577A patent/EP1585001B1/de not_active Expired - Lifetime
- 2005-03-16 AT AT05290577T patent/ATE339716T1/de not_active IP Right Cessation
- 2005-03-16 DE DE602005000123T patent/DE602005000123T2/de not_active Expired - Lifetime
- 2005-03-16 ES ES05290577T patent/ES2273320T3/es not_active Expired - Lifetime
- 2005-03-23 CA CA2500841A patent/CA2500841C/fr not_active Expired - Fee Related
- 2005-04-06 US US11/099,675 patent/US7422176B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| ES2273320T3 (es) | 2007-05-01 |
| US20050269448A1 (en) | 2005-12-08 |
| US7422176B2 (en) | 2008-09-09 |
| DE602005000123D1 (de) | 2006-10-26 |
| EP1585001A1 (de) | 2005-10-12 |
| FR2868852B1 (fr) | 2006-06-30 |
| DE602005000123T2 (de) | 2007-03-01 |
| EP1585001B1 (de) | 2006-09-13 |
| CA2500841A1 (fr) | 2005-10-09 |
| CA2500841C (fr) | 2012-01-03 |
| FR2868852A1 (fr) | 2005-10-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |