DE3687278T2 - Sink-flugbahnregelung fuer flugzeuge. - Google Patents

Sink-flugbahnregelung fuer flugzeuge.

Info

Publication number
DE3687278T2
DE3687278T2 DE8686300034T DE3687278T DE3687278T2 DE 3687278 T2 DE3687278 T2 DE 3687278T2 DE 8686300034 T DE8686300034 T DE 8686300034T DE 3687278 T DE3687278 T DE 3687278T DE 3687278 T2 DE3687278 T2 DE 3687278T2
Authority
DE
Germany
Prior art keywords
aircraft
sink
track control
flight track
flight
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
DE8686300034T
Other languages
English (en)
Other versions
DE3687278D1 (de
Inventor
Terry L Zweifel
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 DE3687278D1 publication Critical patent/DE3687278D1/de
Application granted granted Critical
Publication of DE3687278T2 publication Critical patent/DE3687278T2/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, 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
    • 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
    • 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
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing

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)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE8686300034T 1985-01-09 1986-01-06 Sink-flugbahnregelung fuer flugzeuge. Expired - Fee Related DE3687278T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/689,760 US4709336A (en) 1985-01-09 1985-01-09 Descent flight path control for aircraft

Publications (2)

Publication Number Publication Date
DE3687278D1 DE3687278D1 (de) 1993-01-28
DE3687278T2 true DE3687278T2 (de) 1993-06-03

Family

ID=24769804

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8686300034T Expired - Fee Related DE3687278T2 (de) 1985-01-09 1986-01-06 Sink-flugbahnregelung fuer flugzeuge.

Country Status (5)

Country Link
US (1) US4709336A (de)
EP (1) EP0189239B1 (de)
JP (1) JPS61163096A (de)
CA (1) CA1247218A (de)
DE (1) DE3687278T2 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL87382A (en) * 1987-08-13 1994-07-31 Grumman Aerospace Corp Approach system for accurate landing of aircraft
US5117362A (en) * 1989-12-15 1992-05-26 Honeywell Path capture forcing function generator for aircraft vertical axis control
FR2688077B1 (fr) * 1992-02-28 1994-05-27 Aerospatiale Procede de pilotage d'un avion en mode "maintien de vitesse par action sur la gouverne de profondeur".
SE501815C2 (sv) * 1994-05-30 1995-05-22 Saab Scania Ab Metod och anordning för att utföra faskompensering i ett fordons styrsystem
US5739770A (en) * 1996-01-16 1998-04-14 Honeywell Inc. Off-path descent guidance by a flight management system
FR2863372B1 (fr) * 2003-12-04 2006-02-10 Airbus France Procede et systeme de pilotage automatique d'un aeronef a l'approche d'une position de parachutage.
US7874521B2 (en) 2005-10-17 2011-01-25 Hoshiko Llc Method and system for aviation navigation
US7627403B2 (en) * 2006-03-23 2009-12-01 The Boeing Company Bias correcting phase compensating rate limiter
EP2151730A1 (de) * 2008-08-05 2010-02-10 The Boeing Company Vierdimensionale Flugzeugnavigation
EP2224305B1 (de) * 2009-02-25 2011-10-12 The Boeing Company Implementierung kontinuierlicher Landeanflüge für maximale Vorhersagbarkeit bei Flugzeugen
US8321071B2 (en) * 2009-07-31 2012-11-27 Ge Aviation Systems, Llc Method and system for vertical navigation using time-of-arrival control
US8311687B2 (en) * 2010-07-30 2012-11-13 Ge Aviation Systems Llc Method and system for vertical navigation using time-of-arrival control
US8800936B2 (en) 2011-01-14 2014-08-12 Aerovironment, Inc. Unmanned aerial vehicle drag augmentation by reverse propeller rotation
US8666567B2 (en) 2011-03-31 2014-03-04 Honeywell International Inc. Systems and methods for controlling the speed of an aircraft
FR3005759B1 (fr) * 2013-05-17 2015-06-05 Airbus Operations Sas Procede et dispositif de determination automatique d'un profil optimise d'approche pour un aeronef.
US9646505B2 (en) 2014-12-23 2017-05-09 Ge Aviation Systems Llc Method of automatically controlling the descent phase of an aircraft using aircraft avionics executing a descent algorithm
FR3033925B1 (fr) * 2015-03-16 2017-04-21 Dassault Aviat Procede et systeme de determination d'une trajectoire verticale d'un aeronef
US11358733B2 (en) 2020-01-21 2022-06-14 Rockwell Collins, Inc. Optimum idle descent start point display based on current conditions
US11644340B2 (en) 2021-01-04 2023-05-09 Garmin International, Inc. Automated avionics systems and methods for determining a modified path of descent of an aircraft

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666929A (en) * 1969-09-02 1972-05-30 Lear Siegler Inc Flight control system for following multi-stage descent profile
US3875379A (en) * 1971-05-03 1975-04-01 Carl W Vietor Terminal airways traffic control system
US3868497A (en) * 1971-05-03 1975-02-25 Carl W Vietor Terminal airways traffic control system
US3752967A (en) * 1971-12-20 1973-08-14 C Vietor Ascent and descent slope tracker system
US4021009A (en) * 1975-07-24 1977-05-03 Sperry Rand Corporation Vertical path control for aircraft area navigation system
US4357661A (en) * 1980-02-22 1982-11-02 The Boeing Company Aircraft landing control system
US4413320A (en) * 1980-08-22 1983-11-01 The Bendix Corporation Control system
FR2532079A1 (fr) * 1982-08-18 1984-02-24 Sfena Procede et dispositif de pilotage d'un aerodyne dans le plan vertical, permettant la capture et le maintien d'une vitesse selectee, puis la transition vers une capture d'altitude
US4471439A (en) * 1982-09-20 1984-09-11 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
US4633404A (en) * 1983-05-20 1986-12-30 Sperry Corporation Automatic deceleration of aircraft during descent

Also Published As

Publication number Publication date
US4709336A (en) 1987-11-24
DE3687278D1 (de) 1993-01-28
EP0189239A2 (de) 1986-07-30
JPS61163096A (ja) 1986-07-23
EP0189239A3 (en) 1987-05-20
CA1247218A (en) 1988-12-20
EP0189239B1 (de) 1992-12-16

Similar Documents

Publication Publication Date Title
DE3687278T2 (de) Sink-flugbahnregelung fuer flugzeuge.
DE3576318D1 (de) Ultraleichtflugzeug mit freilaufendem starrfluegel.
DE3480879D1 (de) Flugkontrollsystem fuer hubschrauber.
DE3679486D1 (de) Verstellbares sitzsystem fuer ein flugzeug.
DE3674155D1 (de) Zirkulationsgesteuertes rotorsystem fuer luftfahrzeuge.
DE3669851D1 (de) Tragflaeche.
DE3881667D1 (de) Steuerungssystem fuer hubschrauber.
DE3673243D1 (de) Zweifrequenzinstrumentenlandesystem.
DE3686321D1 (de) Ausstossantrieb fuer flugkoerper.
DE3677315D1 (de) Flugzeugsteuersystem.
DE3480738D1 (de) Geschwindigkeitssteuerung fuer ein flugzeug.
DE3683480D1 (de) Instrument-landungssystem.
DE3786731T2 (de) Kollektivsteuersystem fuer hubschrauber.
DE3682552D1 (de) Flugparameterabhaengige sinkgeschwindigkeitswarnvorrichtung fuer flugzeuge.
DE3686169D1 (de) Einbausysteme fuer fluegelsegelleisten.
IT1188695B (it) Controllo per eliche da aereo
DE3789097D1 (de) Flugsteuersysteme für Hubschrauber.
DE3764336D1 (de) Elektrisches flugsteuerungssystem mit einfallsprotektion fuer luftfahrzeuge.
IT8553439V0 (it) Elicottero
ES2020942B3 (es) Mando para control de velocidad.
DE3669475D1 (de) Flugregelsystem.
DE3685247D1 (de) Flugsteuerungsvorrichtung.
KR870700547A (ko) 비행기 날개
IT8621961A0 (it) Dispositivo di sospensione su aeromobili.
IT1184557B (it) Sistema di controllo antighiaccio per eliche di aeromobili

Legal Events

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