FR1475065A - Aircraft instrument to provide a polarization signal to compensate for the effects of gust components acting forward during approach to landings - Google Patents

Aircraft instrument to provide a polarization signal to compensate for the effects of gust components acting forward during approach to landings

Info

Publication number
FR1475065A
FR1475065A FR51729A FR75051729A FR1475065A FR 1475065 A FR1475065 A FR 1475065A FR 51729 A FR51729 A FR 51729A FR 75051729 A FR75051729 A FR 75051729A FR 1475065 A FR1475065 A FR 1475065A
Authority
FR
France
Prior art keywords
gust
landings
compensate
effects
polarization signal
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
FR51729A
Other languages
French (fr)
Inventor
Leonard Michael Greene
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=23734875&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=FR1475065(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed filed Critical
Application granted granted Critical
Publication of FR1475065A publication Critical patent/FR1475065A/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
    • G05D1/0623—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 Or Direction (AREA)
  • Toys (AREA)
FR51729A 1965-03-04 1966-03-02 Aircraft instrument to provide a polarization signal to compensate for the effects of gust components acting forward during approach to landings Expired FR1475065A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US437055A US3327972A (en) 1965-03-04 1965-03-04 Airplane instrument for furnishing a bias signal to offset the effects of forward components of gusts during landing approach

Publications (1)

Publication Number Publication Date
FR1475065A true FR1475065A (en) 1967-03-31

Family

ID=23734875

Family Applications (1)

Application Number Title Priority Date Filing Date
FR51729A Expired FR1475065A (en) 1965-03-04 1966-03-02 Aircraft instrument to provide a polarization signal to compensate for the effects of gust components acting forward during approach to landings

Country Status (3)

Country Link
US (1) US3327972A (en)
FR (1) FR1475065A (en)
GB (1) GB1101317A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2331027A1 (en) * 1975-11-05 1977-06-03 Safe Flight Instrument GALE INDICATOR DEVICE
EP0005662A1 (en) * 1978-05-08 1979-11-28 Societe Francaise D'equipements Pour La Navigation Aerienne (S.F.E.N.A.) Device for rapidly detecting a wind gradient

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3448947A (en) * 1967-01-30 1969-06-10 Us Navy Fuel throttling computer
DE1802255C2 (en) * 1968-10-10 1971-01-21 Bodenseewerk Geraetetech Speed regulator for aircraft
DE1802518B1 (en) * 1968-10-11 1970-04-09 Bodenseewerk Geraetetech Speed regulator for aircraft
US3662976A (en) * 1969-05-07 1972-05-16 Bodenseewerk Geraetetech Speed controller for aircraft
US3735340A (en) * 1970-04-10 1973-05-22 American Aviat Corp Stall warning system utilizing an electronic time delay
US3892374A (en) * 1973-03-19 1975-07-01 Boeing Co Turbulence compensated throttle control system
US3998411A (en) * 1976-02-17 1976-12-21 Mcdonnell Douglas Corporation Speed overshoot correction system
US4043194A (en) * 1976-08-20 1977-08-23 Tanner Jesse H Wind shear warning system
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
US4646243A (en) * 1983-01-13 1987-02-24 The Boeing Company Apparatus for determining the groundspeed rate of an aircraft
US4855738A (en) * 1987-07-31 1989-08-08 Safe Flight Instrument Corporation Variable threshold wind shear warning system
USRE34082E (en) * 1987-07-31 1992-09-29 Safe Flight Instrument Corporation Variable threshold wind shear warning system
EP0377231A3 (en) * 1989-01-06 1990-08-08 The Boeing Company Method and apparatus for reducing false wind shear alerts
US5590853A (en) * 1992-02-03 1997-01-07 Safe Flight Instrument Corporation Aircraft control system
US5359888A (en) * 1993-02-16 1994-11-01 The B. F. Goodrich Company Air turbulence and wind shear sensor
US8275496B2 (en) * 2007-11-21 2012-09-25 The Boeing Company Longitudinal and vertical gust feed forward compensation using lateral control surfaces

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128967A (en) * 1964-04-14 Command
US2538303A (en) * 1944-03-22 1951-01-16 Robert C Brown Jr Means for determining aerodynamic states of aircraft
US2507367A (en) * 1944-04-01 1950-05-09 Square D Co Instrument for correlating angle of attack and air speed
US2799461A (en) * 1954-05-28 1957-07-16 Collins Radio Co Automatic air speed control
US3143319A (en) * 1960-02-26 1964-08-04 Smiths America Corp Apparatus for the control of an aircraft's speed

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2331027A1 (en) * 1975-11-05 1977-06-03 Safe Flight Instrument GALE INDICATOR DEVICE
EP0005662A1 (en) * 1978-05-08 1979-11-28 Societe Francaise D'equipements Pour La Navigation Aerienne (S.F.E.N.A.) Device for rapidly detecting a wind gradient
WO1979001039A1 (en) * 1978-05-08 1979-11-29 Sfena Fast detector of wind gradient
FR2425644A2 (en) * 1978-05-08 1979-12-07 Equip Navigation Aerienne FAST WIND GRADIENT DETECTION METHOD AND SYSTEM

Also Published As

Publication number Publication date
US3327972A (en) 1967-06-27
GB1101317A (en) 1968-01-31

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