DE3869755D1 - Geschwindigkeitsbeziehungssystem fuer die steuerung eines luftfahrzeugs. - Google Patents

Geschwindigkeitsbeziehungssystem fuer die steuerung eines luftfahrzeugs.

Info

Publication number
DE3869755D1
DE3869755D1 DE8888403185T DE3869755T DE3869755D1 DE 3869755 D1 DE3869755 D1 DE 3869755D1 DE 8888403185 T DE8888403185 T DE 8888403185T DE 3869755 T DE3869755 T DE 3869755T DE 3869755 D1 DE3869755 D1 DE 3869755D1
Authority
DE
Germany
Prior art keywords
aircraft
controlling
speed relation
relation system
speed
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
Application number
DE8888403185T
Other languages
English (en)
Inventor
Jean Louis Bonafe
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
Original Assignee
Airbus Group SAS
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 filed Critical Airbus Group SAS
Application granted granted Critical
Publication of DE3869755D1 publication Critical patent/DE3869755D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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 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
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • G05D1/0623—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the pitch

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE8888403185T 1987-12-22 1988-12-14 Geschwindigkeitsbeziehungssystem fuer die steuerung eines luftfahrzeugs. Expired - Fee Related DE3869755D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8717932A FR2624964B1 (fr) 1987-12-22 1987-12-22 Systeme de reference de vitesse pour le pilotage d'un aeronef

Publications (1)

Publication Number Publication Date
DE3869755D1 true DE3869755D1 (de) 1992-05-07

Family

ID=9358163

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8888403185T Expired - Fee Related DE3869755D1 (de) 1987-12-22 1988-12-14 Geschwindigkeitsbeziehungssystem fuer die steuerung eines luftfahrzeugs.

Country Status (4)

Country Link
US (1) US4967363A (de)
EP (1) EP0322282B1 (de)
DE (1) DE3869755D1 (de)
FR (1) FR2624964B1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5746392A (en) * 1995-05-15 1998-05-05 The Boeing Company Autopilot/flight director underspeed protection system
US5833177A (en) * 1995-05-15 1998-11-10 The Boeing Company Autopilot/flight director overspeed protection system
WO1997020734A2 (en) * 1995-12-06 1997-06-12 Mc Donnell Douglas Corporation Flight control system for jet powered tri-mode 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
FR2756634B1 (fr) * 1996-12-02 1999-01-22 Aerospatiale Procede et dispositif pour la detection de rafales de vent vertical et leur application au pilotage d'un aeronef en profondeur
FR2756541B1 (fr) * 1996-12-02 1999-01-22 Aerospatiale Procede pour la protection d'un aeronef contre les rafales de vent vertical et dispositif de pilotage en profondeur mettant en oeuvre ce procede
US6320579B1 (en) * 1998-12-30 2001-11-20 Honeywell International Inc. Cockpit display having 3D flight path error symbology
US6321086B1 (en) * 1999-06-07 2001-11-20 Motorola, Inc. Comparator and methods for voting therewith
US6885917B2 (en) 2002-11-07 2005-04-26 The Boeing Company Enhanced flight control systems and methods for a jet powered tri-mode aircraft
FR2868852B1 (fr) * 2004-04-09 2006-06-30 Airbus France Sas Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse
FR2894046B1 (fr) * 2005-11-28 2008-02-15 Airbus France Sas Procede de detection d'une erreur d'entree d'un des parametres de decollage dans un systeme de management de vol
US8508387B2 (en) 2007-05-24 2013-08-13 Aviation Communication & Surveillance Systems Llc Systems and methods for aircraft windshear detection
ES2632175T3 (es) * 2009-12-21 2017-09-11 The Boeing Company Cálculo y visualización de la velocidad de aviso para control con asimetría de empuje
CA2972498C (en) 2017-06-28 2024-01-23 Bombardier Inc. Takeoff pitch guidance system and method

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3863056A (en) * 1973-06-29 1975-01-28 Coulter Electronics Method and apparatus for multichannel voting
FR2316647A1 (fr) * 1975-07-04 1977-01-28 Sfena Procede et systeme de pilotage utilisant l'energie totale
FR2344063A1 (fr) * 1976-03-10 1977-10-07 Smiths Industries Ltd Circuit numerique de commande a deux voies au moins
US4092578A (en) * 1976-12-03 1978-05-30 Rockwell International Corporation Elimination of voter caused deadzone
US4162438A (en) * 1978-03-27 1979-07-24 Sperry Rand Corporation Dual servo automatic pilot with improved failure monitoring
EP0258498A1 (de) * 1986-09-01 1988-03-09 The Boeing Company Vorrichtung zur Bestimmung der Geschwindigkeitsänderung eines Flugzeuges
EP0229197B1 (de) * 1985-12-18 1990-07-11 The Boeing Company Flugregel- und Anzeigesystem für Windscherung
US4797674A (en) * 1986-02-28 1989-01-10 Honeywill Inc. Flight guidance system for aircraft in windshear
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

Also Published As

Publication number Publication date
FR2624964A1 (fr) 1989-06-23
US4967363A (en) 1990-10-30
EP0322282B1 (de) 1992-04-01
EP0322282A1 (de) 1989-06-28
FR2624964B1 (fr) 1990-06-01

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee