JPS5385099A - Method of approach flight and system for the same - Google Patents

Method of approach flight and system for the same

Info

Publication number
JPS5385099A
JPS5385099A JP15229377A JP15229377A JPS5385099A JP S5385099 A JPS5385099 A JP S5385099A JP 15229377 A JP15229377 A JP 15229377A JP 15229377 A JP15229377 A JP 15229377A JP S5385099 A JPS5385099 A JP S5385099A
Authority
JP
Japan
Prior art keywords
same
approach flight
flight
approach
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.)
Granted
Application number
JP15229377A
Other languages
English (en)
Other versions
JPS636400B2 (ja
Inventor
Etsuchi Burisu Jiyon
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of JPS5385099A publication Critical patent/JPS5385099A/ja
Publication of JPS636400B2 publication Critical patent/JPS636400B2/ja
Granted 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)
JP15229377A 1976-12-17 1977-12-17 Method of approach flight and system for the same Granted JPS5385099A (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 (2)

Publication Number Publication Date
JPS5385099A true JPS5385099A (en) 1978-07-27
JPS636400B2 JPS636400B2 (ja) 1988-02-09

Family

ID=25023531

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15229377A Granted JPS5385099A (en) 1976-12-17 1977-12-17 Method of approach flight and system for the same

Country Status (3)

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

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4857922A (en) * 1983-05-06 1989-08-15 Honeywell Inc. Windshear detection and warning system with evasion command
EP0400691A1 (en) * 1986-02-13 1990-12-05 Sundstrand Data Control, Inc. Wind shear detection and alerting system
EP0400690A1 (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
US4797674A (en) * 1986-02-28 1989-01-10 Honeywill Inc. Flight guidance system for aircraft in windshear
US7394402B2 (en) * 2001-02-02 2008-07-01 Honeywell International Inc. Tailwind alerting system to prevent runway overruns

Also Published As

Publication number Publication date
GB1586839A (en) 1981-03-25
CA1083693A (en) 1980-08-12
JPS636400B2 (ja) 1988-02-09

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