FR2542276B1 - Dispositif de reglage du tangage d'un aeronef pendant des operations de decollage ou de tour de piste - Google Patents

Dispositif de reglage du tangage d'un aeronef pendant des operations de decollage ou de tour de piste

Info

Publication number
FR2542276B1
FR2542276B1 FR8402142A FR8402142A FR2542276B1 FR 2542276 B1 FR2542276 B1 FR 2542276B1 FR 8402142 A FR8402142 A FR 8402142A FR 8402142 A FR8402142 A FR 8402142A FR 2542276 B1 FR2542276 B1 FR 2542276B1
Authority
FR
France
Prior art keywords
tangage
adjusting
aircraft during
during take
runway operations
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
Application number
FR8402142A
Other languages
English (en)
Other versions
FR2542276A1 (fr
Inventor
Leonard M Greene
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.)
Safe Flight Instrument Co
Safe Flight Instrument Corp
Original Assignee
Safe Flight Instrument Co
Safe Flight Instrument Corp
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 Safe Flight Instrument Co, Safe Flight Instrument Corp filed Critical Safe Flight Instrument Co
Publication of FR2542276A1 publication Critical patent/FR2542276A1/fr
Application granted granted Critical
Publication of FR2542276B1 publication Critical patent/FR2542276B1/fr
Expired 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
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Emergency Alarm Devices (AREA)
  • Traffic Control Systems (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Wind Motors (AREA)
  • Alarm Systems (AREA)
FR8402142A 1983-03-09 1984-02-13 Dispositif de reglage du tangage d'un aeronef pendant des operations de decollage ou de tour de piste Expired FR2542276B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/473,594 US4609987A (en) 1983-03-09 1983-03-09 Aircraft guidance system for take off or go-around during severe wind shear

Publications (2)

Publication Number Publication Date
FR2542276A1 FR2542276A1 (fr) 1984-09-14
FR2542276B1 true FR2542276B1 (fr) 1986-10-24

Family

ID=23880209

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8402142A Expired FR2542276B1 (fr) 1983-03-09 1984-02-13 Dispositif de reglage du tangage d'un aeronef pendant des operations de decollage ou de tour de piste

Country Status (7)

Country Link
US (1) US4609987A (fr)
JP (1) JPS59164296A (fr)
BR (1) BR8400673A (fr)
CA (1) CA1205159A (fr)
DE (1) DE3407677A1 (fr)
FR (1) FR2542276B1 (fr)
IL (1) IL70723A (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4797674A (en) * 1986-02-28 1989-01-10 Honeywill Inc. Flight guidance system for aircraft in windshear
US4853861A (en) * 1987-09-01 1989-08-01 Flight Dynamics, Inc. Windshear measurement system
US4841448A (en) * 1987-09-01 1989-06-20 Flight Dynamics, Inc. Windshear flight recovery command system
JPH02501562A (ja) * 1988-04-11 1990-05-31 サンドストランド・データ・コントロール・インコーポレーテッド 失速保護を有するウインド・シア回復案内装置
US5826834A (en) * 1994-10-19 1998-10-27 Honeywell Inc. Self adaptive limiter for automatic control of approach and landing
US7043345B2 (en) * 2003-10-10 2006-05-09 Raytheon Company System and method with adaptive angle-of-attack autopilot
DE202006010806U1 (de) 2006-07-13 2006-10-05 Harting Electronics Gmbh & Co. Kg Andruckvorrichtung für eine Leiterplatte
US8508387B2 (en) 2007-05-24 2013-08-13 Aviation Communication & Surveillance Systems Llc Systems and methods for aircraft windshear detection
BR112012017154B1 (pt) * 2009-12-21 2021-09-28 The Boeing Company Método de controlar a atitude de inclinação de uma aeronave multimotor experimentando assimetria de impulso e sistema para uma aeronave de multimotor
ES2694427T3 (es) * 2013-06-06 2018-12-20 The Boeing Company Método y sistema de control de velocidad de la aeronave

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3143319A (en) * 1960-02-26 1964-08-04 Smiths America Corp Apparatus for the control of an aircraft's speed
US3814912A (en) * 1973-01-04 1974-06-04 Collins Radio Co Gust compensation for angle-of-attack reference aircraft speed control system
US3892374A (en) * 1973-03-19 1975-07-01 Boeing Co Turbulence compensated throttle control system
US3955071A (en) * 1973-11-16 1976-05-04 The Boeing Company Windshear detection system
GB1553407A (en) * 1975-07-04 1979-09-26 Sfena Flying method and system using total energy for an aircraft
US3981442A (en) * 1975-08-15 1976-09-21 Sperry Rand Corporation Aircraft engine automatic throttle control with automatic gain programming system
US4021010A (en) * 1975-08-29 1977-05-03 Bliss John H Method and apparatus to overcome aircraft control problems due to wind shear
US4189118A (en) * 1977-11-22 1980-02-19 The Boeing Company Shear detection and compensation circuit for aircraft throttle control system
US4212444A (en) * 1977-11-22 1980-07-15 The Boeing Company Gust bias signal-generating circuit for aircraft throttle control system
US4189119A (en) * 1977-11-22 1980-02-19 The Boeing Company Turbulence compensated throttle control system
GB2041571A (en) * 1979-02-09 1980-09-10 Boeing Co Shear detection and compensation circuit for aircraft throttle control system
US4347572A (en) * 1979-11-02 1982-08-31 The Boeing Company Method and apparatus for an aircraft climb-out guidance system
US4319219A (en) * 1980-06-30 1982-03-09 The Boeing Company Automatic approach landing and go-around control system for aircraft
US4422147A (en) * 1980-09-08 1983-12-20 The Boeing Company Wind shear responsive turbulence compensated aircraft throttle control system

Also Published As

Publication number Publication date
DE3407677A1 (de) 1984-09-13
FR2542276A1 (fr) 1984-09-14
US4609987A (en) 1986-09-02
JPH0438639B2 (fr) 1992-06-25
BR8400673A (pt) 1985-02-05
IL70723A (en) 1988-08-31
IL70723A0 (en) 1984-04-30
JPS59164296A (ja) 1984-09-17
CA1205159A (fr) 1986-05-27

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Legal Events

Date Code Title Description
ST Notification of lapse