GB1552365A - Method and system for the rapid detection of a windshear - Google Patents

Method and system for the rapid detection of a windshear

Info

Publication number
GB1552365A
GB1552365A GB50022/76A GB5002276A GB1552365A GB 1552365 A GB1552365 A GB 1552365A GB 50022/76 A GB50022/76 A GB 50022/76A GB 5002276 A GB5002276 A GB 5002276A GB 1552365 A GB1552365 A GB 1552365A
Authority
GB
United Kingdom
Prior art keywords
windshear
rapid detection
rapid
detection
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
GB50022/76A
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.)
Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
Original Assignee
Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
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 Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA filed Critical Societe Francaise dEquipements pour la Navigation Aerienne SFENA SA
Publication of GB1552365A publication Critical patent/GB1552365A/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 or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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

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)
  • Emergency Alarm Devices (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
GB50022/76A 1975-12-03 1976-12-01 Method and system for the rapid detection of a windshear Expired GB1552365A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7536988A FR2334110A1 (en) 1975-12-03 1975-12-03 FAST WIND GRADIENT DETECTION METHOD AND SYSTEM

Publications (1)

Publication Number Publication Date
GB1552365A true GB1552365A (en) 1979-09-12

Family

ID=9163268

Family Applications (1)

Application Number Title Priority Date Filing Date
GB50022/76A Expired GB1552365A (en) 1975-12-03 1976-12-01 Method and system for the rapid detection of a windshear

Country Status (5)

Country Link
CA (1) CA1102450A (en)
DE (1) DE2655370C2 (en)
FR (1) FR2334110A1 (en)
GB (1) GB1552365A (en)
IT (1) IT1074617B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4178406A (en) * 1977-12-29 1979-12-11 Rohm And Haas Company Three-layered fiberglass construction
JPS57191198A (en) * 1981-03-02 1982-11-24 Sperry Rand Corp Detecting and alarming device for window shear
FR2756634B1 (en) * 1996-12-02 1999-01-22 Aerospatiale METHOD AND DEVICE FOR THE DETECTION OF VERTICAL WIND GUSTS AND THEIR APPLICATION TO THE PILOTAGE OF AN AIRCRAFT IN DEPTH
FR2756644B1 (en) * 1997-04-16 1999-01-22 Aerospatiale METHOD AND DEVICE FOR THE DETECTION OF VERTICAL WIND GUSTS AND ON APPLICATION TO THE PILOTAGE OF AN AIRCRAFT IN DEPTH
EP4227214A4 (en) * 2020-11-13 2024-02-28 Mitsubishi Heavy Ind Ltd Aircraft control system, aircraft, aircraft control method, and program

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3840200A (en) * 1973-03-19 1974-10-08 Boeing Co Turbulence compensated throttle control system

Also Published As

Publication number Publication date
FR2334110A1 (en) 1977-07-01
DE2655370C2 (en) 1986-11-06
FR2334110B1 (en) 1980-05-09
CA1102450A (en) 1981-06-02
IT1074617B (en) 1985-04-20
DE2655370A1 (en) 1977-06-08

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19931201