FR2450198A1 - Circuit de detection et de compensation de cisaillement du vent - Google Patents

Circuit de detection et de compensation de cisaillement du vent

Info

Publication number
FR2450198A1
FR2450198A1 FR7905277A FR7905277A FR2450198A1 FR 2450198 A1 FR2450198 A1 FR 2450198A1 FR 7905277 A FR7905277 A FR 7905277A FR 7905277 A FR7905277 A FR 7905277A FR 2450198 A1 FR2450198 A1 FR 2450198A1
Authority
FR
France
Prior art keywords
compensator
incorporates
control system
throttle control
speed variation
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
FR7905277A
Other languages
English (en)
French (fr)
Other versions
FR2450198B1 (enrdf_load_stackoverflow
Inventor
Henri Peter-Contesse
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Priority to FR7905277A priority Critical patent/FR2450198A1/fr
Publication of FR2450198A1 publication Critical patent/FR2450198A1/fr
Application granted granted Critical
Publication of FR2450198B1 publication Critical patent/FR2450198B1/fr
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
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Radar Systems Or Details Thereof (AREA)
FR7905277A 1979-02-28 1979-02-28 Circuit de detection et de compensation de cisaillement du vent Granted FR2450198A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7905277A FR2450198A1 (fr) 1979-02-28 1979-02-28 Circuit de detection et de compensation de cisaillement du vent

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7905277A FR2450198A1 (fr) 1979-02-28 1979-02-28 Circuit de detection et de compensation de cisaillement du vent

Publications (2)

Publication Number Publication Date
FR2450198A1 true FR2450198A1 (fr) 1980-09-26
FR2450198B1 FR2450198B1 (enrdf_load_stackoverflow) 1984-10-19

Family

ID=9222602

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7905277A Granted FR2450198A1 (fr) 1979-02-28 1979-02-28 Circuit de detection et de compensation de cisaillement du vent

Country Status (1)

Country Link
FR (1) FR2450198A1 (enrdf_load_stackoverflow)

Citations (2)

* 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
US4209152A (en) * 1977-11-25 1980-06-24 The Boeing Company Turbulence compensated throttle control system for aircraft having throttle command signal path control means responsive to engine rating control and flare initiation

Patent Citations (2)

* 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
US4209152A (en) * 1977-11-25 1980-06-24 The Boeing Company Turbulence compensated throttle control system for aircraft having throttle command signal path control means responsive to engine rating control and flare initiation

Also Published As

Publication number Publication date
FR2450198B1 (enrdf_load_stackoverflow) 1984-10-19

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Legal Events

Date Code Title Description
ST Notification of lapse