ES2173402T3 - Dispositivo para mantener la velocidad de una aeronave dentro de un margen de velocidades determinado. - Google Patents

Dispositivo para mantener la velocidad de una aeronave dentro de un margen de velocidades determinado.

Info

Publication number
ES2173402T3
ES2173402T3 ES97400656T ES97400656T ES2173402T3 ES 2173402 T3 ES2173402 T3 ES 2173402T3 ES 97400656 T ES97400656 T ES 97400656T ES 97400656 T ES97400656 T ES 97400656T ES 2173402 T3 ES2173402 T3 ES 2173402T3
Authority
ES
Spain
Prior art keywords
aircraft
speed
maintaining
margin
determined
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
Application number
ES97400656T
Other languages
English (en)
Inventor
Claude Maffre
Jean Muller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aerospatiale Matra
Original Assignee
Aerospatiale Matra
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Aerospatiale Matra filed Critical Aerospatiale Matra
Application granted granted Critical
Publication of ES2173402T3 publication Critical patent/ES2173402T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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

Abstract

LA PRESENTE INVENCION SE REFIERE A UN DISPOSITIVO AUTOMATICO PARA MANTENER UNA AERONAVE A UNA VELOCIDAD AUTORIZADA COMPATIBLE CON LAS CAPACIDADES TECNICAS DE DICHA AERONAVE. SEGUN LA INVENCION, DICHO DISPOSITIVO (1) LLEVA: - MEDIOS (11,13) PARA COMPARAR LA VELOCIDAD EFECTIVA DE LA AERONAVE CON VELOCIDADES DE REFERENCIA DEFINIDAS EN FUNCION DE LAS CAPACIDADES TECNICAS DE DICHA AERONAVE; - MEDIOS (9) PARA CALCULAR, EN FUNCION DE LAS COMPARACIONES, VALORES DE CONTROL MODIFICADOS SUSCEPTIBLES DE ALINEAR LA VELOCIDAD EFECTIVA CON ESTAS VELOCIDADES DE REFERENCIA; Y - MEDIOS (10) PARA IMPONER A LA AERONAVE UNO DE ESTOS VALORES CALCULADOS, SI ESTO ES NECESARIO PARA MANTENER LA AERONAVE A UNA VELOCIDAD AUTORIZADA.
ES97400656T 1996-04-05 1997-03-24 Dispositivo para mantener la velocidad de una aeronave dentro de un margen de velocidades determinado. Expired - Lifetime ES2173402T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9604311A FR2747204B1 (fr) 1996-04-05 1996-04-05 Dispositif pour maintenir la vitesse d'un aeronef a l'interieur d'un domaine de vitesses determine

Publications (1)

Publication Number Publication Date
ES2173402T3 true ES2173402T3 (es) 2002-10-16

Family

ID=9490964

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97400656T Expired - Lifetime ES2173402T3 (es) 1996-04-05 1997-03-24 Dispositivo para mantener la velocidad de una aeronave dentro de un margen de velocidades determinado.

Country Status (7)

Country Link
US (1) US5884870A (es)
EP (1) EP0799766B1 (es)
CN (1) CN1134721C (es)
CA (1) CA2201078C (es)
DE (1) DE69712399T2 (es)
ES (1) ES2173402T3 (es)
FR (1) FR2747204B1 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2002324927A1 (en) * 2001-09-13 2003-03-24 Brian E. Turung Airplane emergency navigational system
US8103589B2 (en) * 2002-09-16 2012-01-24 Touchtunes Music Corporation Digital downloading jukebox system with central and local music servers
US7715431B1 (en) * 2002-10-16 2010-05-11 Cisco Technology, Inc. Fallback for V.42 modem-over-internet-protocol (MoIP) gateways method and apparatus
FR2868852B1 (fr) * 2004-04-09 2006-06-30 Airbus France Sas Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse
ES2304815B1 (es) * 2005-01-26 2009-10-21 INSTITUTO NACIONAL DE TECNICA AEROESPACIAL "ESTEBAN TERRADAS" Metodo para el control de parametros de control en un vehiculo aereo, y sistema de control de un vehiculo aereo.
FR2889162B1 (fr) * 2005-07-28 2007-09-07 Airbus France Sas Procede et dispositif de pilotage d'un aeronef selon au moins un axe de pilotage
CN100519337C (zh) * 2005-09-12 2009-07-29 贝尔直升机泰克斯特龙公司 飞行器以及飞行器的自动速度控制系统和方法
US9235217B2 (en) * 2005-10-03 2016-01-12 Sikorsky Aircraft Corporation Automatic dual rotor speed control for helicopters
FR2903379B1 (fr) 2006-07-07 2008-08-29 Thales Sa Convertisseur de commande de facteur de charge en consigne d'ecart d'assiette longitudinale
FR2907541B1 (fr) * 2006-10-24 2009-01-16 Thales Sa Procede de gestion automatique de la vitesse d'un aeronef en air turbulent et dispositif pour sa mise en oeuvre
FR3033908B1 (fr) * 2015-03-18 2018-11-30 Dassault Aviation Systeme et procede d'assistance au pilotage d'un aeronef
FR3038585B1 (fr) 2015-07-10 2017-08-18 Dassault Aviat Systeme de pilotage automatique d'aeronef et procede associe
CN105005342B (zh) * 2015-08-11 2017-06-16 中国航空工业集团公司西安飞机设计研究所 控制飞行器自动起飞的方法
CN107305393A (zh) * 2016-04-20 2017-10-31 比亚迪股份有限公司 无人机及其控制方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3860800A (en) * 1972-06-19 1975-01-14 Boeing Co Automatic pitch axis control system for aircraft
US4044975A (en) * 1976-05-17 1977-08-30 Mcdonnell Douglas Corporation Aircraft speed command system
US5031102A (en) * 1979-12-03 1991-07-09 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
WO1984001345A1 (en) * 1982-09-30 1984-04-12 Boeing Co Total energy based flight control system
US4577275A (en) * 1983-05-31 1986-03-18 United Technologies Corporation Flight director go-around mode
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
US4841448A (en) * 1987-09-01 1989-06-20 Flight Dynamics, Inc. Windshear flight recovery command system
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
US5225829A (en) * 1991-05-09 1993-07-06 Sundstrand Corporation Independent low airspeed alert
US5730394A (en) * 1995-12-20 1998-03-24 Sikorsky Aircraft Corporation Vertical performance limit compensator

Also Published As

Publication number Publication date
CA2201078A1 (fr) 1997-10-05
FR2747204A1 (fr) 1997-10-10
DE69712399T2 (de) 2002-12-12
US5884870A (en) 1999-03-23
CN1173652A (zh) 1998-02-18
CN1134721C (zh) 2004-01-14
EP0799766B1 (fr) 2002-05-08
FR2747204B1 (fr) 1998-06-12
DE69712399D1 (de) 2002-06-13
CA2201078C (fr) 2005-08-16
EP0799766A1 (fr) 1997-10-08

Similar Documents

Publication Publication Date Title
ES2173402T3 (es) Dispositivo para mantener la velocidad de una aeronave dentro de un margen de velocidades determinado.
SE9603336D0 (sv) System med optisk förstärkare
ATE306413T1 (de) Stellwerkanlage für eisenbahnen
MX161780A (es) Mejoras en aparato controlador de interruptor
DK0462124T3 (da) Fremgangsmåde samt arrangement til betjening af en koblingsregulator
DK415683A (da) Reguleringsmekanisme til regulering af effekten hos en forbraendingsmotor
HUP9903719A2 (hu) Eljárás egyenáramú hajtás vezérlésére
SE8301026L (sv) Kopplingsanordning for styrning av rorelsen for en instellningsanordning, i synnerhet en patientstol
ES2088635T3 (es) Sistema/metodo protector de la seccion divisora sincronizada.
FR2702575B1 (fr) Dispositif de controle de la rotation d'au moins un organe de reglage.
BR9811162A (pt) Processo de controlar a velocidade de um veìculo, e, sistema de controle de velocidade de cruzeiro de um veìculo
FI903960A0 (fi) Foerfarande foer styrning av en elapparat.
DK271889D0 (da) Laegemiddel paa basis af en aryloxypropanolamin til selektiv antagonisering af 5-ht1-receptorer
DE3864891D1 (de) Verfahren und einrichtung zur wegregelung eines positionsantriebes.
DE59305899D1 (de) Interferometrisches messverfahren sowie für seine durchführung geeignete laserinterferometeranordnung
DE69200584D1 (de) Einrichtung zur Drehzahlsteuerung eines Flugzeugtriebwerkes.
DK0491200T3 (da) Fremgangsmåde til styring af en kranmotor
SE9803918D0 (sv) Säkring av järnvägsövergång
FR2703902B1 (fr) Tête de contre-angle pour instrument endodontique.
ATE322614T1 (de) Fliehkraftdrehzahlregler
ATA67296A (de) Richtmaschine
DE69212152T2 (de) Kransteuerungsverfahren
SU952666A1 (ru) Устройство задани режимов работы тиристорно-импульсного регул тора привода двигател транспортного средства
BR0009508B1 (pt) processo e dispositivo para a regulaÇço de uma turbina a vapor com tomada de vapor.
DE69916533D1 (de) Mäh- und Konditionierungsvorrichtung

Legal Events

Date Code Title Description
FG2A Definitive protection

Ref document number: 799766

Country of ref document: ES