ES2017738B3 - Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave. - Google Patents

Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave.

Info

Publication number
ES2017738B3
ES2017738B3 ES87401976T ES87401976T ES2017738B3 ES 2017738 B3 ES2017738 B3 ES 2017738B3 ES 87401976 T ES87401976 T ES 87401976T ES 87401976 T ES87401976 T ES 87401976T ES 2017738 B3 ES2017738 B3 ES 2017738B3
Authority
ES
Spain
Prior art keywords
aircraft
control system
flight control
electric flight
incidence protection
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
ES87401976T
Other languages
English (en)
Inventor
Pierre Fabre
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.)
Airbus Group SAS
Aerospatiale Matra
Original Assignee
Airbus Group SAS
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 Airbus Group SAS, Aerospatiale Matra filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2017738B3 publication Critical patent/ES2017738B3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Radar Systems Or Details Thereof (AREA)
ES87401976T 1986-09-15 1987-09-03 Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave. Expired - Lifetime ES2017738B3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8612855A FR2604001B1 (fr) 1986-09-15 1986-09-15 Systeme de commande de vol electrique avec protection en incidence pour aeronef

Publications (1)

Publication Number Publication Date
ES2017738B3 true ES2017738B3 (es) 1991-03-01

Family

ID=9338935

Family Applications (1)

Application Number Title Priority Date Filing Date
ES87401976T Expired - Lifetime ES2017738B3 (es) 1986-09-15 1987-09-03 Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave.

Country Status (6)

Country Link
US (1) US4829220A (es)
EP (1) EP0261015B1 (es)
CA (1) CA1270563A (es)
DE (1) DE3764336D1 (es)
ES (1) ES2017738B3 (es)
FR (1) FR2604001B1 (es)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01185709A (ja) * 1988-01-20 1989-07-25 Teijin Seiki Co Ltd 故障検出機構付きサーボ回路
FR2661149B1 (fr) * 1990-04-24 1992-08-14 Aerospatiale Systeme pour le pilotage d'un avion en tangage.
FR2711257B1 (fr) * 1993-10-14 1995-12-22 Aerospatiale Système de commande de vol électrique pour avion avec protection en assiette au décollage.
US5746392A (en) † 1995-05-15 1998-05-05 The Boeing Company Autopilot/flight director underspeed protection system
US5803408A (en) * 1995-05-15 1998-09-08 The Boeing Company Autopilot/flight director stall protection system
FR2826469B1 (fr) 2001-06-25 2003-10-24 Eads Airbus Sa Procede et dispositif pour commander au moins une surface aerodynamique de profondeur d'un avion lors d'un decollage
FR2866627B1 (fr) * 2004-02-24 2006-05-05 Airbus France Procede et dispositif pour l'optimisation du braquage des volets deporteurs d'un aeronef en vol
DE102004045732A1 (de) * 2004-09-21 2006-03-30 Airbus Deutschland Gmbh Flugzeug mit Flügeln, deren maximaler Auftrieb durch steuerbare Flügelkomponenten veränderbar ist
CN102219051B (zh) * 2011-04-29 2013-01-09 北京工业大学 基于人机交互技术的四旋翼飞行器系统控制方法
EP2551737B1 (en) * 2011-07-28 2015-04-29 Airbus Defence and Space GmbH Method and apparatus for minimizing dynamic structural loads of an aircraft
US9845146B2 (en) * 2015-10-23 2017-12-19 The Boeing Company Zoom climb prevention system for enhanced performance
DE102016117638B4 (de) * 2016-09-19 2018-05-24 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verminderung von an einem Luftfahrzeug auftretenden Böenlasten
US11841713B2 (en) * 2020-01-07 2023-12-12 Gulfstream Aerospace Corporation Controllers and aircraft with takeoff stall protection system

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3393380A (en) * 1966-03-15 1968-07-16 James E. Webb Phase locked phase modulator including a voltage controlled oscillator
CH601874A5 (es) * 1976-07-07 1978-07-14 Bbc Brown Boveri & Cie
US4052672A (en) * 1976-07-22 1977-10-04 Motorola, Inc. Extended phase-range, high fidelity modulator arrangement
US4110707A (en) * 1976-12-13 1978-08-29 Texas Instruments Incorporated Indirect FM modulation scheme using phase locked loop
DE2807902C2 (de) * 1978-02-24 1980-04-30 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Steuereinrichtung mit aktiver Kraft rückführung
US4304375A (en) * 1979-05-17 1981-12-08 Textron Inc. Electrically controlled elevator
CA1158219A (en) * 1980-04-01 1983-12-06 Edmond D. Diamond Multi-axis force stick, self-trimmed aircraft flight control system
EP0120855B1 (en) * 1982-09-30 1989-01-25 The Boeing Company Total energy based flight control system
US4500857A (en) * 1983-02-24 1985-02-19 The United States Of America As Represented By The Secretary Of The Army Frequency modulated phase locked loop
DE3462866D1 (en) * 1984-01-09 1987-05-07 Aerospatiale Aircraft flight control system

Also Published As

Publication number Publication date
EP0261015B1 (fr) 1990-08-16
US4829220A (en) 1989-05-09
FR2604001A1 (fr) 1988-03-18
FR2604001B1 (fr) 1988-12-09
DE3764336D1 (de) 1990-09-20
EP0261015A1 (fr) 1988-03-23
CA1270563A (fr) 1990-06-19

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