ES2051089T3 - Sistema para el pilotaje de un avion en cabeceo. - Google Patents
Sistema para el pilotaje de un avion en cabeceo.Info
- Publication number
- ES2051089T3 ES2051089T3 ES91401045T ES91401045T ES2051089T3 ES 2051089 T3 ES2051089 T3 ES 2051089T3 ES 91401045 T ES91401045 T ES 91401045T ES 91401045 T ES91401045 T ES 91401045T ES 2051089 T3 ES2051089 T3 ES 2051089T3
- Authority
- ES
- Spain
- Prior art keywords
- delta
- adjustable
- command order
- horizontal plane
- aircraft
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/503—Fly-by-Wire
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/506—Transmitting means with power amplification using electrical energy overriding of personal controls; with automatic return to inoperative position
-
- 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
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Traffic Control Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
- Mechanical Control Devices (AREA)
Abstract
A UN NUMERO DE MACH SUPERIOR A 0,7 Y QUE COMPRENDE UN PLANO HORIZONTAL (6) AJUSTABLE EN DESVIACION Y AEROFRENOS (5) DE EFECTO PICADOR. OS MEDIOS (10) QUE PROPORCIONAN, A CADA INSTANTE, LA INCIDENCIA AERODINAMICA ((ALFA)) DE DICHO AVION (1); 12) QUE GENERAN, EN CASO DE QUE DICHA INADENCIA AERODINAMICA SEA SUPERIOR A DICHO PRIMER UMBRAL ((ALFA)O), UNA PRIMERA ORDEN DE MANDO DE PICAR (DELTA IHC) PARA DICHO PLANO HORIZONTAL AJUSTABLE (6), LA AMPLITUD DE DICHO PRIMERA ORDEN DE MANDO ES TAL QUE; SI DICHO PLANO HORIZONTAL AJUSTABLE TOMASE INSTANTANEAMENTE LA POSICION CORRESPONDIENTE, COMPENSARIA EL AUMENTO DE ENCABRITADO DE DICHO AVION DEBIDO AL COMPORTAMIENTO DE LA VARIACION DE DICHO PAR AERODINAMICO DE CABECEO POR ENCIMA DE DICHO PRIMER UMBRAL IHE) REPRESENTATIVO DE RESPUESTA EN DESVIACION EN FUNCION DEL TIEMPO, DE DICHO PLANO HORIZONTAL AJUSTABLE A DICHA PRIMERA ORDEN DE MANDO; D(DELTA IH) ENTRE DICHA PRIMERA ORDEN DE MANDO (DELTA IHC) Y DICHA SEÑAL (DELTA IHE) REPRESENTATIVA DE LA RESPUESTA DEDICHO PLANO HORIZONTAL AJUSTABLE; Y AR, A PARTIR DE DICHA DIFERENCIA D(DELTA IH), UNA SEGUNDA ORDEN DE MANDO DE PICAR PARA DICHOS AEROFRENOS PICADORES (5).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9005227A FR2661149B1 (fr) | 1990-04-24 | 1990-04-24 | Systeme pour le pilotage d'un avion en tangage. |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2051089T3 true ES2051089T3 (es) | 1994-06-01 |
Family
ID=9396042
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES91401045T Expired - Lifetime ES2051089T3 (es) | 1990-04-24 | 1991-04-19 | Sistema para el pilotaje de un avion en cabeceo. |
Country Status (6)
Country | Link |
---|---|
US (1) | US5112009A (es) |
EP (1) | EP0454549B1 (es) |
CA (1) | CA2040874C (es) |
DE (1) | DE69101154T2 (es) |
ES (1) | ES2051089T3 (es) |
FR (1) | FR2661149B1 (es) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2694738B1 (fr) * | 1992-08-14 | 1994-11-10 | Aerospatiale | Procédé de commande des gouvernes d'un avion pour compenser à basse vitesse une déviation latérale de trajectoire. |
FR2719548B1 (fr) * | 1994-05-03 | 1996-07-05 | Aerospatiale | Avion de transport à empennage avant. |
US5779191A (en) * | 1996-11-12 | 1998-07-14 | Brislawn; Mark G. | Pylon flap for increasing negative pitching moments |
US7802756B2 (en) * | 2000-02-14 | 2010-09-28 | Aerovironment Inc. | Aircraft control system |
US6641086B2 (en) * | 2001-08-14 | 2003-11-04 | Northrop Grumman Corporation | System and method for controlling an aircraft |
US20050242234A1 (en) * | 2004-04-29 | 2005-11-03 | The Boeing Company | Lifters, methods of flight control and maneuver load alleviation |
FR2870819B1 (fr) * | 2004-05-28 | 2006-08-25 | Airbus France Sas | Systeme de commande des aerofreins d'un avion |
CA2568848C (en) * | 2004-07-16 | 2013-06-25 | Airbus France | Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out |
FR2881849B1 (fr) * | 2005-02-04 | 2007-04-06 | Airbus France Sas | Procede et dispositif de pilotage d'un avion en tangage |
FR2893909B1 (fr) * | 2005-11-29 | 2007-12-21 | Airbus France Sas | Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse. |
GB2444742B (en) * | 2006-12-11 | 2011-06-08 | Embraer Aeronautica Sa | Flight Control System |
DE102007012425A1 (de) * | 2007-03-15 | 2008-09-18 | Airbus Deutschland Gmbh | Verfahren und Einrichtung zur Höhenflossentrimmung bei einem Flugzeug |
RU2445671C2 (ru) * | 2010-02-25 | 2012-03-20 | Московский государственный университет приборостроения и информатики | Система адаптивного управления самолетом по углу тангажа |
US8666567B2 (en) * | 2011-03-31 | 2014-03-04 | Honeywell International Inc. | Systems and methods for controlling the speed of an aircraft |
FR3002334B1 (fr) * | 2013-02-19 | 2016-07-15 | Airbus Operations Sas | Procede et dispositif d'estimation d'un moment de tangage non desire d'un avion, et applications au controle du tangage de l'avion. |
US9731813B2 (en) * | 2014-11-12 | 2017-08-15 | The Boeing Company | Methods and apparatus to control aircraft horizontal stabilizers |
FR3057370B1 (fr) * | 2016-10-11 | 2019-08-23 | Airbus Operations | Procede et systeme de commande de vol d'un aeronef. |
CN108628342A (zh) * | 2018-04-28 | 2018-10-09 | 长光卫星技术有限公司 | 无人飞行器的自动飞行控制***及方法 |
CN114056551B (zh) * | 2022-01-12 | 2022-04-01 | 中国空气动力研究与发展中心低速空气动力研究所 | 虚拟腹襟翼、翼身融合飞机、定常吹气及变角吹气的方法 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3167276A (en) * | 1961-09-29 | 1965-01-26 | Honeywell Inc | Control apparatus |
US3142457A (en) * | 1962-07-16 | 1964-07-28 | Boeing Co | Stall pattern lift regulator for airplanes |
US3942746A (en) * | 1971-12-27 | 1976-03-09 | General Dynamics Corporation | Aircraft having improved performance with beaver-tail afterbody configuration |
US4003533A (en) * | 1973-10-01 | 1977-01-18 | General Dynamics Corporation | Combination airbrake and pitch control device |
US4142699A (en) * | 1977-02-04 | 1979-03-06 | Boeing Commercial Airplane Company | Lateral control system |
US4261537A (en) * | 1979-02-28 | 1981-04-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Velocity vector control system augmented with direct lift control |
US4304375A (en) * | 1979-05-17 | 1981-12-08 | Textron Inc. | Electrically controlled elevator |
US4442490A (en) * | 1980-09-26 | 1984-04-10 | S-Tec Corporation | Aircraft pitch stabilization apparatus |
US4485446A (en) * | 1981-09-08 | 1984-11-27 | The Boeing Company | Aircraft lift control system with acceleration and attitude limiting |
US4569494A (en) * | 1982-12-23 | 1986-02-11 | The Boeing Company | Pitch control of swept wing aircraft |
DE3462866D1 (en) * | 1984-01-09 | 1987-05-07 | Aerospatiale | Aircraft flight control system |
FR2604001B1 (fr) * | 1986-09-15 | 1988-12-09 | Aerospatiale | Systeme de commande de vol electrique avec protection en incidence pour aeronef |
US4956780A (en) * | 1988-12-08 | 1990-09-11 | The Boeing Company | Flight path angle command flight control system for landing flare |
-
1990
- 1990-04-24 FR FR9005227A patent/FR2661149B1/fr not_active Expired - Lifetime
-
1991
- 1991-04-19 EP EP91401045A patent/EP0454549B1/fr not_active Expired - Lifetime
- 1991-04-19 CA CA002040874A patent/CA2040874C/fr not_active Expired - Lifetime
- 1991-04-19 ES ES91401045T patent/ES2051089T3/es not_active Expired - Lifetime
- 1991-04-19 DE DE69101154T patent/DE69101154T2/de not_active Expired - Lifetime
- 1991-04-24 US US07/690,310 patent/US5112009A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5112009A (en) | 1992-05-12 |
CA2040874A1 (fr) | 1991-10-25 |
FR2661149A1 (fr) | 1991-10-25 |
DE69101154T2 (de) | 1994-07-21 |
EP0454549A1 (fr) | 1991-10-30 |
FR2661149B1 (fr) | 1992-08-14 |
CA2040874C (fr) | 2001-06-12 |
DE69101154D1 (de) | 1994-03-24 |
EP0454549B1 (fr) | 1994-02-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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