ATE458984T1 - Umsetzer zum umsetzen eines lastfaktorbefehls in eine longitudinal-lageabweichungsanweisung - Google Patents
Umsetzer zum umsetzen eines lastfaktorbefehls in eine longitudinal-lageabweichungsanweisungInfo
- Publication number
- ATE458984T1 ATE458984T1 AT07730261T AT07730261T ATE458984T1 AT E458984 T1 ATE458984 T1 AT E458984T1 AT 07730261 T AT07730261 T AT 07730261T AT 07730261 T AT07730261 T AT 07730261T AT E458984 T1 ATE458984 T1 AT E458984T1
- Authority
- AT
- Austria
- Prior art keywords
- load factor
- command
- converter
- converting
- longitudinal attitude
- Prior art date
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 abstract 1
- 230000010354 integration Effects 0.000 abstract 1
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
- 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
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Navigation (AREA)
- Feedback Control In General (AREA)
- General Induction Heating (AREA)
- Control Of Electric Motors In General (AREA)
- Diaphragms For Electromechanical Transducers (AREA)
- Magnetic Resonance Imaging Apparatus (AREA)
- Hydraulic Control Valves For Brake Systems (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0606221A FR2903379B1 (fr) | 2006-07-07 | 2006-07-07 | Convertisseur de commande de facteur de charge en consigne d'ecart d'assiette longitudinale |
PCT/EP2007/056125 WO2008003591A1 (fr) | 2006-07-07 | 2007-06-20 | Convertisseur de commande de facteur de charge en consigne d'ecart d'assiette longitudinale |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE458984T1 true ATE458984T1 (de) | 2010-03-15 |
Family
ID=38001814
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT07730261T ATE458984T1 (de) | 2006-07-07 | 2007-06-20 | Umsetzer zum umsetzen eines lastfaktorbefehls in eine longitudinal-lageabweichungsanweisung |
Country Status (7)
Country | Link |
---|---|
US (1) | US8046118B2 (de) |
EP (1) | EP2038613B1 (de) |
AT (1) | ATE458984T1 (de) |
DE (1) | DE602007004988D1 (de) |
ES (1) | ES2339604T3 (de) |
FR (1) | FR2903379B1 (de) |
WO (1) | WO2008003591A1 (de) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140343765A1 (en) | 2012-12-28 | 2014-11-20 | Sean Patrick Suiter | Flight Assistant with Automatic Configuration and Landing Site Selection |
FR3008499B1 (fr) * | 2013-07-12 | 2015-08-07 | Airbus Operations Sas | Procede et dispositif d'affichage en temps reel d'une consigne d'assiette sur un aeronef lors d'un pilotage manuel. |
FR3057370B1 (fr) * | 2016-10-11 | 2019-08-23 | Airbus Operations | Procede et systeme de commande de vol d'un aeronef. |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2668750B1 (fr) * | 1990-11-06 | 1993-01-22 | Aerospatiale | Systeme pour la commande integree en profondeur et en poussee d'un aeronef. |
US5213282A (en) * | 1991-08-28 | 1993-05-25 | United Technologies Corporation | Maneuver feel system for a rotary wing aircraft |
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 |
US5823479A (en) * | 1996-05-20 | 1998-10-20 | The Boeing Company | Landing attitude modifier for airplane |
US6273370B1 (en) * | 1999-11-01 | 2001-08-14 | Lockheed Martin Corporation | Method and system for estimation and correction of angle-of-attack and sideslip angle from acceleration measurements |
US6735500B2 (en) * | 2002-06-10 | 2004-05-11 | The Boeing Company | Method, system, and computer program product for tactile cueing flight control |
FR2841008B1 (fr) * | 2002-06-12 | 2004-08-20 | Airbus France | Procede et systeme de pilotage d'un aeronef |
FR2874204B1 (fr) * | 2004-08-13 | 2007-12-14 | Airbus France Sas | Systeme de commande de vol electriques pour les gouvernes de profondeur d'un aeronef |
-
2006
- 2006-07-07 FR FR0606221A patent/FR2903379B1/fr not_active Expired - Fee Related
-
2007
- 2007-06-20 ES ES07730261T patent/ES2339604T3/es active Active
- 2007-06-20 US US12/307,221 patent/US8046118B2/en not_active Expired - Fee Related
- 2007-06-20 DE DE602007004988T patent/DE602007004988D1/de not_active Expired - Fee Related
- 2007-06-20 WO PCT/EP2007/056125 patent/WO2008003591A1/fr active Application Filing
- 2007-06-20 EP EP07730261A patent/EP2038613B1/de not_active Not-in-force
- 2007-06-20 AT AT07730261T patent/ATE458984T1/de not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
WO2008003591A1 (fr) | 2008-01-10 |
US8046118B2 (en) | 2011-10-25 |
FR2903379B1 (fr) | 2008-08-29 |
FR2903379A1 (fr) | 2008-01-11 |
ES2339604T3 (es) | 2010-05-21 |
DE602007004988D1 (de) | 2010-04-08 |
EP2038613B1 (de) | 2010-02-24 |
US20090287365A1 (en) | 2009-11-19 |
EP2038613A1 (de) | 2009-03-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |