GB1586839A - Apparatus to overcome aircraft control problems due to wind shear - Google Patents

Apparatus to overcome aircraft control problems due to wind shear Download PDF

Info

Publication number
GB1586839A
GB1586839A GB51281/77A GB5128177A GB1586839A GB 1586839 A GB1586839 A GB 1586839A GB 51281/77 A GB51281/77 A GB 51281/77A GB 5128177 A GB5128177 A GB 5128177A GB 1586839 A GB1586839 A GB 1586839A
Authority
GB
United Kingdom
Prior art keywords
index
groundspeed
aircraft
airspeed
tas
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
GB51281/77A
Other languages
English (en)
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.)
Bliss J H
Original Assignee
Bliss J H
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
Priority claimed from US05/751,801 external-priority patent/US4133503A/en
Application filed by Bliss J H filed Critical Bliss J H
Publication of GB1586839A publication Critical patent/GB1586839A/en
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
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • G05D1/063—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the motors
    • 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)
  • Navigation (AREA)
GB51281/77A 1976-12-17 1977-12-09 Apparatus to overcome aircraft control problems due to wind shear Expired GB1586839A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/751,801 US4133503A (en) 1975-08-29 1976-12-17 Entry, display and use of data employed to overcome aircraft control problems due to wind shear

Publications (1)

Publication Number Publication Date
GB1586839A true GB1586839A (en) 1981-03-25

Family

ID=25023531

Family Applications (1)

Application Number Title Priority Date Filing Date
GB51281/77A Expired GB1586839A (en) 1976-12-17 1977-12-09 Apparatus to overcome aircraft control problems due to wind shear

Country Status (3)

Country Link
JP (1) JPS5385099A (enrdf_load_stackoverflow)
CA (1) CA1083693A (enrdf_load_stackoverflow)
GB (1) GB1586839A (enrdf_load_stackoverflow)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0235964A3 (en) * 1986-02-28 1988-09-07 Honeywell Inc. Method and apparatus for flight guidance for an aircraft in windshear
EP0235962A3 (en) * 1986-02-28 1988-09-07 Honeywell Inc. Windshear detection and warning system
EP0400690A1 (en) * 1986-02-13 1990-12-05 Sundstrand Data Control, Inc. Wind shear detection and alerting system
EP0400691A1 (en) * 1986-02-13 1990-12-05 Sundstrand Data Control, Inc. Wind shear detection and alerting system
EP0401877A1 (en) * 1986-02-13 1990-12-12 Sundstrand Data Control, Inc. Wind shear detection and alerting system
WO2006101806A1 (en) * 2005-03-23 2006-09-28 Honeywell Inc. Tailwind alerting system to prevent runway overruns

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0400690A1 (en) * 1986-02-13 1990-12-05 Sundstrand Data Control, Inc. Wind shear detection and alerting system
EP0400691A1 (en) * 1986-02-13 1990-12-05 Sundstrand Data Control, Inc. Wind shear detection and alerting system
EP0401877A1 (en) * 1986-02-13 1990-12-12 Sundstrand Data Control, Inc. Wind shear detection and alerting system
EP0235964A3 (en) * 1986-02-28 1988-09-07 Honeywell Inc. Method and apparatus for flight guidance for an aircraft in windshear
EP0235962A3 (en) * 1986-02-28 1988-09-07 Honeywell Inc. Windshear detection and warning system
US7394402B2 (en) 2001-02-02 2008-07-01 Honeywell International Inc. Tailwind alerting system to prevent runway overruns
WO2006101806A1 (en) * 2005-03-23 2006-09-28 Honeywell Inc. Tailwind alerting system to prevent runway overruns

Also Published As

Publication number Publication date
JPS636400B2 (enrdf_load_stackoverflow) 1988-02-09
JPS5385099A (en) 1978-07-27
CA1083693A (en) 1980-08-12

Similar Documents

Publication Publication Date Title
US4133503A (en) Entry, display and use of data employed to overcome aircraft control problems due to wind shear
US4106731A (en) Method and apparatus to overcome aircraft control problems due to wind shear
US4825374A (en) Aircraft descent guide system and method for creating descent guidance information
US4019702A (en) Method and apparatus for guiding a jet aircraft in a noise-abated post-takeoff climb
EP2589538B1 (en) Display device, piloting assistance system, and display method
JP4328660B2 (ja) 航空機の自動離陸装置、自動着陸装置及び自動離着陸装置並びに航空機の自動離陸方法、自動着陸方法及び自動離着陸方法
EP2573522B1 (en) An aircraft speed guidance display
US4786905A (en) Wind shear detector head-up display system
GB1405236A (en) Apparatus for controlling the flight of a vertical or short take- off and landing craft
US3496769A (en) Descent-approach system for aircraft
RU2267747C1 (ru) Способ управления самолетом при заходе на посадку
JPH0524589A (ja) 垂直離着陸航空機の自動着陸誘導方法
US2892180A (en) Aircraft flight instrument
GB1586839A (en) Apparatus to overcome aircraft control problems due to wind shear
US4004758A (en) Method and apparatus for providing decelerated aircraft approach
US2143137A (en) System for piloting aircraft
GB913840A (en) Improvements in or relating to airborne glide slope director systems
RU2478523C2 (ru) Способ управления самолетом при заходе на посадку
Sadraey Flight Path Control Systems
Smith et al. A flight investigation of a terminal area navigation and guidance concept for STOL aircraft
Adams Flight-test verification of a pictorial display for general aviation instrument approach
GB950863A (en) Improvements in or relating to automatic landing systems for aircraft
Lennox Part II: Approach Guidance
Moseley et al. Historic paper on automatic radio flight control
GB1415692A (en) Aircraft instruments

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PE20 Patent expired after termination of 20 years

Effective date: 19960818