ES2044918T3 - Metodo y apparato para dirigir el vuelo de un avion en cortante del viento. - Google Patents

Metodo y apparato para dirigir el vuelo de un avion en cortante del viento.

Info

Publication number
ES2044918T3
ES2044918T3 ES87301013T ES87301013T ES2044918T3 ES 2044918 T3 ES2044918 T3 ES 2044918T3 ES 87301013 T ES87301013 T ES 87301013T ES 87301013 T ES87301013 T ES 87301013T ES 2044918 T3 ES2044918 T3 ES 2044918T3
Authority
ES
Spain
Prior art keywords
air
speed
aircraft
command
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 - Lifetime
Application number
ES87301013T
Other languages
English (en)
Inventor
Terry L Zweifel
David Alan Johnson
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
Application granted granted Critical
Publication of ES2044918T3 publication Critical patent/ES2044918T3/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
    • 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)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Control Of Velocity Or Acceleration (AREA)
  • Navigation (AREA)

Abstract

METODO Y APARATO PARA COMANDAR UNA VIA DE VUELO OPTIMO PARA UN AVION EN CONDICIONES DE BACHES DE AIRE. UNA SEÑAL DEL RANGO DE LA VELOCIDAD DEL AIRE IGUAL EN MAGNITUD Y EN SENTIDO OPUESTO AL BACHE DE AIRE SE APLICA PARA DERIVAR UNA PROPORCION VARIABLE DE CAMBIO DE COMANDO DE VELOCIDAD DEL AIRE PARA SU APLICACION EN UN INDICADOR DIRECTOR DE VUELO (57, 140). SE COLOCAN LIMITES EN LOS COMANDOS DE DERIVA DE TAL MANERA QUE EL COMANDO DE VELOCIDAD MINIMA PERMITIDA ES LA VELOCIDAD DE VIBRACION Y LA MAXIMA LA VELOCIDAD NOMINAL EN AUSENCIA DE BACHES DE AIRE. LA SEÑAL DE COMANDO RESULTANTE REPRESENTA UNA PROPORCION DE VELOCIDAD DEL AIRE REAL QUE PRODUCE UN CAMINO DE VUELO OPTIMO PARA QUE EL AVION SALGA DE LAS CONDICIONES DE BACHES DE AIRE.
ES87301013T 1986-02-28 1987-02-05 Metodo y apparato para dirigir el vuelo de un avion en cortante del viento. Expired - Lifetime ES2044918T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/834,729 US4797674A (en) 1986-02-28 1986-02-28 Flight guidance system for aircraft in windshear

Publications (1)

Publication Number Publication Date
ES2044918T3 true ES2044918T3 (es) 1994-01-16

Family

ID=25267646

Family Applications (1)

Application Number Title Priority Date Filing Date
ES87301013T Expired - Lifetime ES2044918T3 (es) 1986-02-28 1987-02-05 Metodo y apparato para dirigir el vuelo de un avion en cortante del viento.

Country Status (7)

Country Link
US (1) US4797674A (es)
EP (1) EP0235964B1 (es)
JP (1) JPS62206414A (es)
BR (1) BR8605895A (es)
CA (1) CA1270545A (es)
DE (1) DE3787741T2 (es)
ES (1) ES2044918T3 (es)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2038993T3 (es) * 1987-11-27 1993-08-16 Honeywell Inc. Guia optima de vuelo para un avion en una rafaga de viento.
FR2624964B1 (fr) * 1987-12-22 1990-06-01 Aerospatiale Systeme de reference de vitesse pour le pilotage d'un aeronef
US4891642A (en) * 1988-01-11 1990-01-02 Sundstrand Data Control, Inc. Wind shear detection system
US4893245A (en) * 1988-01-11 1990-01-09 Honeywell Inc. Windshear guidance for aircraft having inertial sensor
EP0368989A4 (en) * 1988-04-11 1990-06-26 Sundstrand Data Control SYSTEM FOR WINCH SHEAR INTERCEPTIONS WITH STABLE PROTECTION.
EP0377231A3 (en) * 1989-01-06 1990-08-08 The Boeing Company Method and apparatus for reducing false wind shear alerts
US5053767A (en) * 1990-03-12 1991-10-01 Honeywell Inc. Aircraft windshear detection based on energy loss
US5187477A (en) * 1990-04-10 1993-02-16 Sundstrand Corporation Wind shear detector with slow shear bias
US5361065A (en) * 1990-05-11 1994-11-01 Honeywell Inc. Windshear guidance system
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
US6970107B2 (en) * 2003-07-29 2005-11-29 Gannett James R Flight situation presentation system and method
WO2007005045A2 (en) * 2004-10-08 2007-01-11 Bell Helicopter Textron, Inc. Control system for automatic flight in windshear conditions
FR2891802B1 (fr) * 2005-10-11 2009-03-13 Airbus France Sas Procede et dispositif pour attenuer sur un aeronef les effets d'une turbulence verticale
US7557735B1 (en) 2006-09-05 2009-07-07 Rockwell Collins, Inc. Predictive and reactive windshear detection system and method
US8494766B2 (en) 2011-01-07 2013-07-23 Ge Aviation Systems, Llc Flight management system with integrated tactical commands for use with an aircraft and method of operating same
US9424753B2 (en) 2011-07-08 2016-08-23 General Electric Company Simplified user interface for an aircraft
US10338090B2 (en) * 2014-09-04 2019-07-02 Sikorsky Aircraft Corporation Airspeed estimation system
US11841713B2 (en) * 2020-01-07 2023-12-12 Gulfstream Aerospace Corporation Controllers and aircraft with takeoff stall protection system
CN114789798B (zh) * 2022-06-27 2022-10-25 成都飞机工业（集团）有限责任公司 一种飞机舱门阶差预测方法、装置、设备及介质

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3839699A (en) * 1969-08-05 1974-10-01 Monitair Corp Aircraft stall warning indicator system based on rate of change of angle of attack
US3686626A (en) * 1970-06-03 1972-08-22 United Control Corp Aircraft instrument
US3822047A (en) * 1972-12-14 1974-07-02 Collins Radio Co Takeoff and go-around climb-out profile pitch command formulation for aircraft
US3840200A (en) * 1973-03-19 1974-10-08 Boeing Co Turbulence compensated throttle control system
US4044975A (en) * 1976-05-17 1977-08-30 Mcdonnell Douglas Corporation Aircraft speed command system
GB1586839A (en) * 1976-12-17 1981-03-25 Bliss John H Apparatus to overcome aircraft control problems due to wind shear
US4079905A (en) * 1977-02-07 1978-03-21 Safe Flight Instrument Corporation System for providing an indication of wind shear
US4189777A (en) * 1978-05-01 1980-02-19 The Bendix Corporation Ground proximity warning system with means for altering warning threshold in accordance with wind shear
US4229725A (en) * 1978-05-12 1980-10-21 Reilly Richard J Wind shear warning system for aircraft
US4347572A (en) * 1979-11-02 1982-08-31 The Boeing Company Method and apparatus for an aircraft climb-out guidance system
US4326253A (en) * 1980-03-31 1982-04-20 The Boeing Company Lift control system for aircraft vertical path guidance
US4319219A (en) * 1980-06-30 1982-03-09 The Boeing Company Automatic approach landing and go-around control system for aircraft
US4536843A (en) * 1982-09-30 1985-08-20 The Boeing Company Total energy based flight control system
US4609987A (en) * 1983-03-09 1986-09-02 Safe Flight Instrument Corporation Aircraft guidance system for take off or go-around during severe wind shear
US4593285A (en) * 1983-05-06 1986-06-03 Sperry Corporation Windshear detection and warning system with evasion command
DE3578659D1 (de) * 1985-12-18 1990-08-16 Boeing Co Flugregel- und anzeigesystem fuer windscherung.

Also Published As

Publication number Publication date
EP0235964B1 (en) 1993-10-13
EP0235964A2 (en) 1987-09-09
DE3787741D1 (de) 1993-11-18
EP0235964A3 (en) 1988-09-07
US4797674A (en) 1989-01-10
JPS62206414A (ja) 1987-09-10
BR8605895A (pt) 1987-09-08
DE3787741T2 (de) 1994-02-24
CA1270545A (en) 1990-06-19

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