DE3785101T2 - System zum steuern des vertikalen flugweges und der fluggeschwindigkeit eines flugzeuges. - Google Patents

System zum steuern des vertikalen flugweges und der fluggeschwindigkeit eines flugzeuges.

Info

Publication number
DE3785101T2
DE3785101T2 DE8787306190T DE3785101T DE3785101T2 DE 3785101 T2 DE3785101 T2 DE 3785101T2 DE 8787306190 T DE8787306190 T DE 8787306190T DE 3785101 T DE3785101 T DE 3785101T DE 3785101 T2 DE3785101 T2 DE 3785101T2
Authority
DE
Germany
Prior art keywords
airplane
controlling
vertical
speed
airplane 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
DE8787306190T
Other languages
English (en)
Other versions
DE3785101D1 (de
Inventor
Harry Miller
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.)
Honeywell Inc
Original Assignee
Honeywell Inc
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 Honeywell Inc filed Critical Honeywell Inc
Publication of DE3785101D1 publication Critical patent/DE3785101D1/de
Application granted granted Critical
Publication of DE3785101T2 publication Critical patent/DE3785101T2/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
    • G05D1/0638—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by combined action on the pitch and on the motors
DE8787306190T 1986-07-16 1987-07-13 System zum steuern des vertikalen flugweges und der fluggeschwindigkeit eines flugzeuges. Expired - Fee Related DE3785101T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/886,127 US4764872A (en) 1986-07-16 1986-07-16 Vertical flight path and airspeed control system for aircraft

Publications (2)

Publication Number Publication Date
DE3785101D1 DE3785101D1 (de) 1993-05-06
DE3785101T2 true DE3785101T2 (de) 1993-09-16

Family

ID=25388432

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787306190T Expired - Fee Related DE3785101T2 (de) 1986-07-16 1987-07-13 System zum steuern des vertikalen flugweges und der fluggeschwindigkeit eines flugzeuges.

Country Status (4)

Country Link
US (1) US4764872A (de)
EP (1) EP0253614B1 (de)
JP (1) JPS6325198A (de)
DE (1) DE3785101T2 (de)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2624964B1 (fr) * 1987-12-22 1990-06-01 Aerospatiale Systeme de reference de vitesse pour le pilotage d'un aeronef
US5103224A (en) * 1990-02-16 1992-04-07 Ady Arad Aircraft takeoff monitoring system
US5056027A (en) * 1990-02-26 1991-10-08 Honeywell Inc. Apparatus and method for a smooth transition between calibrated airspeed control of an aircraft and mach number control of an aircraft
US5079711A (en) * 1990-02-26 1992-01-07 The Boeing Company Aircraft high altitude vertical flight path and speed control system
FR2664231B1 (fr) * 1990-07-04 1992-10-09 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
US5096146A (en) * 1990-08-17 1992-03-17 The Boeing Company Apparatus and methods for controlling commanded operation of an aircraft within a predetermined flight parameter limit
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
US5478031A (en) * 1993-09-29 1995-12-26 Rockwell International Corporation Airspeed control system which utilizes pitch hold command when pilot throttle changes oppose elevator control
US5826834A (en) * 1994-10-19 1998-10-27 Honeywell Inc. Self adaptive limiter for automatic control of approach and landing
US5667166A (en) * 1995-01-12 1997-09-16 The Boeing Company Aircraft frequency adaptive modal suppression system
US5833177A (en) * 1995-05-15 1998-11-10 The Boeing Company Autopilot/flight director overspeed protection system
US5746392A (en) * 1995-05-15 1998-05-05 The Boeing Company Autopilot/flight director underspeed protection system
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
US6041273A (en) * 1997-07-01 2000-03-21 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Emergency control aircraft system using thrust modulation
US6186447B1 (en) * 1997-11-10 2001-02-13 The Boeing Company Autothrottle retard rate control system
US6062513A (en) * 1998-09-14 2000-05-16 The Boeing Company Total energy based flight control system
FR2831871B1 (fr) * 2001-11-08 2004-08-13 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef
FR2845350B1 (fr) * 2002-10-02 2004-12-17 Airbus France Procede et dispositif pour commander automatiquement la pousse d'au moins un moteur d'un aeronef lors d'une phase de vol horizontal a vitesse stabilisee
US6814330B2 (en) * 2002-12-12 2004-11-09 The Boeing Company Method and computer program product for controlling the control effectors of an aerodynamic vehicle
US7031811B2 (en) * 2003-05-30 2006-04-18 The Boeing Company Fuel efficient airspeed trim
US7177785B2 (en) * 2003-08-22 2007-02-13 Honeywell International, Inc. Systems and methods for improved aircraft performance predictions
FR2859787B1 (fr) * 2003-09-16 2006-01-20 Thales Sa Dispositif et procede de determination de la temperature totale pour aeronef
US7046193B2 (en) * 2003-11-24 2006-05-16 Honeywell International Inc. Software GPS based integrated navigation
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.
EP2151730A1 (de) * 2008-08-05 2010-02-10 The Boeing Company Vierdimensionale Flugzeugnavigation
EP2282247B1 (de) * 2009-05-05 2019-07-10 The Boeing Company Vierdimensionale Lenkung eines Flugzeugs
US8321071B2 (en) * 2009-07-31 2012-11-27 Ge Aviation Systems, Llc Method and system for vertical navigation using time-of-arrival control
FR2959316B1 (fr) * 2010-04-21 2012-05-18 Airbus Operations Sas Procede et dispositif d'estimation automatique d'une vitesse air d'un avion
ES2485294T3 (es) * 2010-08-24 2014-08-13 The Boeing Company Guiado en cuatro dimensiones de una aeronave
FR2977948B1 (fr) * 2011-07-12 2014-11-07 Eurocopter France Procede de pilotage automatique d'un aeronef a voilure tournante comprenant au moins une helice propulsive, dispositif de pilotage automatique et aeronef
US9828113B2 (en) 2013-11-05 2017-11-28 Safe Flight Instrument Corporation Tailstrike warning system
JP6267945B2 (ja) * 2013-11-25 2018-01-24 三菱航空機株式会社 航空機のエンジン制御コンピュータ、および航空機
US9546003B2 (en) 2014-03-14 2017-01-17 Safe Flight Instrument Corporation Deflare pitch command
US9346552B2 (en) * 2014-04-11 2016-05-24 Safe Flight Instrument Corporation Autothrottle retard control
FR3033908B1 (fr) * 2015-03-18 2018-11-30 Dassault Aviation Systeme et procede d'assistance au pilotage d'un aeronef
US20170008639A1 (en) 2015-07-08 2017-01-12 Safe Flight Instrument Corporation Aircraft turbulence detection
CA2972498C (en) 2017-06-28 2024-01-23 Bombardier Inc. Takeoff pitch guidance system and method
FR3075994B1 (fr) * 2017-12-21 2023-11-24 Airbus Operations Sas Procede d'aide au pilotage d'un aeronef, permettant d'assurer la disponibilite d'un pilote automatique ou d'un regulateur de la poussee
US20230205229A1 (en) * 2021-12-23 2023-06-29 Electra Aero, Inc. System and method for controlling flight path of a blown lift aircraft

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3618878A (en) * 1969-06-23 1971-11-09 Lear Siegler Inc Aircraft throttle control
US3691356A (en) * 1970-12-10 1972-09-12 Sperry Rand Corp Speed command and throttle control system for aircraft
US3945593A (en) * 1972-10-10 1976-03-23 Bodenseewerk Geratetechnik Gmbh Flight control apparatus
US3901466A (en) * 1972-11-16 1975-08-26 Boeing Co Thrust and flight path control decoupling system
US3981442A (en) * 1975-08-15 1976-09-21 Sperry Rand Corporation Aircraft engine automatic throttle control with automatic gain programming system
US4488235A (en) * 1981-11-03 1984-12-11 Sperry Corporation Speed control system for aircraft
US4490793A (en) * 1981-12-21 1984-12-25 Sperry Corporation Cruise speed control for aircraft performance management system
US4471439A (en) * 1982-09-20 1984-09-11 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
DE3279390D1 (en) * 1982-09-30 1989-03-02 Boeing Co Total energy based flight control system
US4641268A (en) * 1983-01-27 1987-02-03 Sperry Corporation Cruise airspeed control for aircraft
US4589616A (en) * 1984-01-24 1986-05-20 Sperry Corporation Cruise airspeed control of aircraft altitude capture

Also Published As

Publication number Publication date
EP0253614B1 (de) 1993-03-31
DE3785101D1 (de) 1993-05-06
JPS6325198A (ja) 1988-02-02
EP0253614A2 (de) 1988-01-20
US4764872A (en) 1988-08-16
EP0253614A3 (en) 1989-08-23

Similar Documents

Publication Publication Date Title
DE3785101T2 (de) System zum steuern des vertikalen flugweges und der fluggeschwindigkeit eines flugzeuges.
DE3774751D1 (de) System zum herstellen von kontinuierlichen langen keramischen gegenstaenden.
DE3869394D1 (de) Einrichtung zum thermischen zerlegen von fluiden schadstoffen.
DE68922192D1 (de) System zum Überwachen der Entfernung von Gegenständen.
DE3785827D1 (de) System zum regeln des zapfens.
DE3761211D1 (de) Klappe zum automatischen regulieren des niveaus.
DE3777835D1 (de) Nichtverunreinigendes system zum sichtbarmachen von stroemung.
DE3770209D1 (de) Vorrichtung zum ueberfuehren von bahnen.
DE3884063T2 (de) Gerät zum Folgen des Sonnenlichtes.
NO871480D0 (no) Apparat for stoeping av termoplastroer.
DK631487D0 (da) Benzofuran- eller thiophenderivat samt fremgangsmaade til fremstilling deraf
DE3765237D1 (de) Vorrichtung zum regeln der fuellhoehe.
DE195721T1 (de) Vorrichtung zum verhindern des aushaengens von schiebetueren.
DE3771088D1 (de) Haengefoerdersystem und angepasstes betriebsmittel.
DE68924972T2 (de) Steuerungssystem des Antriebs eines Luftfahrzeugs.
DE3786527T2 (de) Gerät zum Steuern von externen Ausrüstungen.
DE68912050T2 (de) Einrichtung zum Stranggiessen von Metallbändern.
AT397761B (de) Gerät zum behandeln von oberflächen od. dgl.
DE3884827T2 (de) Vorrichtung zum Filtrieren und Reinigungsverfahren der Vorrichtung.
DE3576939D1 (de) Geraet zum halten von fahrzeugen und dergleichen.
DE3784439D1 (de) Einrichtung zum sequenz-strangguss verschiedener stahlzusammensetzungen.
DE3782528T2 (de) Selektive medien zum wachstum von neisseria.
AT383147B (de) Vorrichtung zum plasmaaetzen von leiterplatten od.dgl.
DE3668875D1 (de) Hubmastbefestigungsanordnung und verfahren zum abnehmen des hubmastes.
AT389129B (de) Vorrichtung zum schneefreihalten von eisenbahnweichen

Legal Events

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