FR2835606B1 - Indicateur d'attitude pour aeronef - Google Patents
Indicateur d'attitude pour aeronefInfo
- Publication number
- FR2835606B1 FR2835606B1 FR0201217A FR0201217A FR2835606B1 FR 2835606 B1 FR2835606 B1 FR 2835606B1 FR 0201217 A FR0201217 A FR 0201217A FR 0201217 A FR0201217 A FR 0201217A FR 2835606 B1 FR2835606 B1 FR 2835606B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- attitude indicator
- attitude
- indicator
- 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 - Fee Related
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
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Traffic Control Systems (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
- Level Indicators Using A Float (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0201217A FR2835606B1 (fr) | 2002-02-01 | 2002-02-01 | Indicateur d'attitude pour aeronef |
EP03717362A EP1470391A2 (fr) | 2002-02-01 | 2003-01-31 | Indicateur d attitude pour aeronef |
US10/483,828 US20050012642A1 (en) | 2002-02-01 | 2003-01-31 | Attitude indicator for an aircraft |
CA002457772A CA2457772A1 (fr) | 2002-02-01 | 2003-01-31 | Indicateur d'attitude pour aeronef |
BR0302577-2A BR0302577A (pt) | 2002-02-01 | 2003-01-31 | Indicador de posição para aeronave |
PCT/FR2003/000302 WO2003064976A2 (fr) | 2002-02-01 | 2003-01-31 | Indicateur d'attitude pour aeronef |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0201217A FR2835606B1 (fr) | 2002-02-01 | 2002-02-01 | Indicateur d'attitude pour aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2835606A1 FR2835606A1 (fr) | 2003-08-08 |
FR2835606B1 true FR2835606B1 (fr) | 2006-02-03 |
Family
ID=27619824
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0201217A Expired - Fee Related FR2835606B1 (fr) | 2002-02-01 | 2002-02-01 | Indicateur d'attitude pour aeronef |
Country Status (6)
Country | Link |
---|---|
US (1) | US20050012642A1 (fr) |
EP (1) | EP1470391A2 (fr) |
BR (1) | BR0302577A (fr) |
CA (1) | CA2457772A1 (fr) |
FR (1) | FR2835606B1 (fr) |
WO (1) | WO2003064976A2 (fr) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005108924A1 (fr) * | 2004-04-29 | 2005-11-17 | Jadi, Inc. | Dispositif a horizon artificiel et procede y relatif |
FR2906223B1 (fr) * | 2006-09-22 | 2008-11-21 | Thales Sa | Instrument de secours pour tableau de bord d'un aeronef detectant les surcharges, notamment en phase d'atterrissage |
FR2911115B1 (fr) * | 2007-01-10 | 2009-02-27 | Airbus France Sas | Dispositif d'interconnexion entre un poste de pilotage et au moins une autre zone d'un aeronef, cockpit et aeronef equipes d'un tel dispositif d'interconnexion |
FR2915824B1 (fr) * | 2007-05-02 | 2009-06-05 | Thales Sa | Procede d'optimisation de la sortie d'un aeronef dans un circuit d'attente |
FR2916287B1 (fr) * | 2007-05-15 | 2014-06-27 | Thales Sa | Procede de tracement d'une portion de trajectoire d'un aeronef comprenant un arc de cercle a rayon constant |
FR2919066B1 (fr) * | 2007-07-17 | 2009-11-06 | Thales Sa | Instrument de secours pour aeronef |
US8392039B2 (en) * | 2008-05-29 | 2013-03-05 | Honeywell International Inc. | Method and system displaying crosswind correction for approach to a runway |
US20100030408A1 (en) * | 2008-07-31 | 2010-02-04 | Honeywell International, Inc. | Integrated incorrect take-off-setting alerting system |
US20100179712A1 (en) * | 2009-01-15 | 2010-07-15 | Honeywell International Inc. | Transparent vehicle skin and methods for viewing vehicle systems and operating status |
US8290641B2 (en) | 2009-04-21 | 2012-10-16 | Pilot Disorientation Prevention Technologies, L.L.C. | Aircraft attitude systems and related methods |
US8352099B1 (en) | 2009-07-09 | 2013-01-08 | The Boeing Company | Varying engine thrust for directional control of an aircraft experiencing engine thrust asymmetry |
US20110193725A1 (en) * | 2010-02-11 | 2011-08-11 | Honeywell International Inc. | Methods and systems for displaying a symbol representative of an aircraft in flight |
US8421649B2 (en) | 2010-02-22 | 2013-04-16 | Jerry Lee Marstall | Aircraft attitude systems |
US8462020B1 (en) * | 2010-03-24 | 2013-06-11 | Russell Alan Vanhoozer | Attitude and configuration indicator display system and method |
JP5916283B2 (ja) * | 2010-07-01 | 2016-05-11 | 三菱重工業株式会社 | 表示装置、操縦支援システム、及び表示方法 |
US9221552B2 (en) * | 2012-06-29 | 2015-12-29 | Honeywell International Inc. | Aircraft systems and methods for attitude recovery |
FR3008202B1 (fr) * | 2013-07-05 | 2015-07-17 | Thales Sa | Procede de gestion et de representation d un indicateur de taux de virage pour aeronef |
JP6193691B2 (ja) * | 2013-09-11 | 2017-09-06 | 三菱航空機株式会社 | 防氷システム、及び、航空機 |
FR3045015B1 (fr) * | 2015-12-09 | 2017-12-22 | Thales Sa | Procede d'affichage d'un "indicateur de directeur d'attitude" dans un systeme de visualisation de tete pour aeronef |
FR3046227B1 (fr) * | 2015-12-29 | 2018-01-05 | Thales | Procede de representation graphique de la position relative du ciel et de la terre dans un systeme de visualisation de bord pour aeronef |
EP3339809A1 (fr) * | 2016-12-22 | 2018-06-27 | Ecole Nationale de l'Aviation Civile | Procédé et appareil de commande d'affichage d'attitude d'un véhicule |
CN108983819A (zh) * | 2018-08-14 | 2018-12-11 | 苏敏华 | 一种无人机管控方法、装置及*** |
CN114120792B (zh) * | 2021-11-30 | 2024-02-27 | 中国人民解放军海军航空大学 | 一种基于飞机姿态控制的专用教具 |
US20230259085A1 (en) * | 2022-02-12 | 2023-08-17 | Guy E Mossman | Trim management system |
DE102022116786B4 (de) | 2022-07-05 | 2024-06-13 | Hung-Hsin Lin | Flugzeug-Hilfsanzeigesystem zum Vermeiden Räumlicher Desorientierung |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3579847A (en) * | 1968-05-29 | 1971-05-25 | Aviat Instr Mfg Corp | Attitude indicator |
US4326189A (en) * | 1979-04-23 | 1982-04-20 | Crane Carl J | Aircraft control/guidance display and mechanism for enroute and landing utility |
FR2569840B1 (fr) * | 1984-08-31 | 1986-09-05 | Schnerb Pierre | Dispositif destine a representer sur l'ecran d'un tube de television les deplacements d'un mobile, en vue notamment de faciliter le pilotage des vehicules, en particulier des vehicules aeriens |
DE4314811A1 (de) * | 1993-05-05 | 1994-12-08 | Vdo Luftfahrtgeraete Werk Gmbh | Verfahren zur Darstellung von Flugführungsinformationen |
US6028536A (en) * | 1995-11-16 | 2000-02-22 | Northrop Grumman Corporation | Integrated flight control indicator |
DE19955664C2 (de) * | 1999-11-19 | 2003-07-17 | Eads Deutschland Gmbh | Flugführungs-Display zur Anwendung in Flugzeug-Cockpit und Flugzeug-Simulationssystemen |
-
2002
- 2002-02-01 FR FR0201217A patent/FR2835606B1/fr not_active Expired - Fee Related
-
2003
- 2003-01-31 BR BR0302577-2A patent/BR0302577A/pt not_active Application Discontinuation
- 2003-01-31 EP EP03717362A patent/EP1470391A2/fr not_active Withdrawn
- 2003-01-31 CA CA002457772A patent/CA2457772A1/fr not_active Abandoned
- 2003-01-31 US US10/483,828 patent/US20050012642A1/en not_active Abandoned
- 2003-01-31 WO PCT/FR2003/000302 patent/WO2003064976A2/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
BR0302577A (pt) | 2004-02-25 |
CA2457772A1 (fr) | 2003-08-07 |
WO2003064976A3 (fr) | 2004-04-08 |
US20050012642A1 (en) | 2005-01-20 |
EP1470391A2 (fr) | 2004-10-27 |
FR2835606A1 (fr) | 2003-08-08 |
WO2003064976A2 (fr) | 2003-08-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2835606B1 (fr) | Indicateur d'attitude pour aeronef | |
GB0201148D0 (en) | Navigation system | |
GB0213215D0 (en) | Computer navigation | |
EP1293756A4 (fr) | Dispositif de navigation | |
DE60228514D1 (de) | Integriertes Flugmanagementsystem | |
EP1542721A4 (fr) | Anticorps "s" modifies | |
ITTO20030640A1 (it) | Apparato d'interfaccia uomo- macchina mediante | |
GB0320850D0 (en) | Navigation device | |
GB0103138D0 (en) | Navigation system | |
FI20010429A0 (fi) | Punnitusjärjestelmä | |
FR2847496B1 (fr) | Masselotte utilisee pour la fonderie | |
FR2862279B1 (fr) | Ballon gonflable a facettes pour l'evenementiel | |
FR2845713B1 (fr) | Dispositif pour l'amenagement de locaux polyvalents | |
FR2764863B1 (fr) | Indicateur de position pour aeronef | |
GB0325667D0 (en) | Shave "n" go | |
FR2825444B1 (fr) | Vanne d'aerage | |
FR2831393B1 (fr) | Appat pour bulots ou analogues | |
FR2845349B1 (fr) | Potence pour aeronef | |
FR2830233B1 (fr) | Coque pour structure navigante | |
GB0101311D0 (en) | The global vortal | |
UA6852S (uk) | Коліматорний авіаційний індикатор | |
GB0316880D0 (en) | Draughtsman's scale rule | |
GB0213974D0 (en) | Navigation buoy | |
UA7990S (uk) | Ущільнювач для конструктивного прорізу судна | |
GB0208043D0 (en) | Aircraft compass |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 15 |
|
ST | Notification of lapse |
Effective date: 20171031 |