FR1515275A - Système de commande de vol pour avions ou engins aériens analogues - Google Patents

Système de commande de vol pour avions ou engins aériens analogues

Info

Publication number
FR1515275A
FR1515275A FR92934A FR92934A FR1515275A FR 1515275 A FR1515275 A FR 1515275A FR 92934 A FR92934 A FR 92934A FR 92934 A FR92934 A FR 92934A FR 1515275 A FR1515275 A FR 1515275A
Authority
FR
France
Prior art keywords
airplanes
control system
flight control
aerial vehicles
similar aerial
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
FR92934A
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.)
Allard Way Holdings Ltd
Original Assignee
Elliott Brothers London Ltd
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 Elliott Brothers London Ltd filed Critical Elliott Brothers London Ltd
Application granted granted Critical
Publication of FR1515275A publication Critical patent/FR1515275A/fr
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
    • G05D1/0653—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)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR92934A 1966-01-29 1967-01-30 Système de commande de vol pour avions ou engins aériens analogues Expired FR1515275A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4059/66A GB1178673A (en) 1966-01-29 1966-01-29 Improvements in and relating to the Control of Aircraft

Publications (1)

Publication Number Publication Date
FR1515275A true FR1515275A (fr) 1968-03-01

Family

ID=9769954

Family Applications (1)

Application Number Title Priority Date Filing Date
FR92934A Expired FR1515275A (fr) 1966-01-29 1967-01-30 Système de commande de vol pour avions ou engins aériens analogues

Country Status (3)

Country Link
US (1) US3489378A (fr)
FR (1) FR1515275A (fr)
GB (1) GB1178673A (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1274751A (en) * 1969-01-29 1972-05-17 Elliott Brothers London Ltd Improvements in or relating to automatic flight control systems
US3665465A (en) * 1969-10-22 1972-05-23 Rita Ann Miller Deceleration schedule for aircraft landing
US3652835A (en) * 1970-05-14 1972-03-28 Sperry Rand Corp Aircraft glide slope coupler system
US3773281A (en) * 1971-06-18 1973-11-20 Bendix Corp Automatic flight control system using instrument landing system information and including inertial filtering means for reducing ils noise
US4164340A (en) * 1973-03-19 1979-08-14 The Boeing Company Method and apparatus for determining when a glide slope signal exceeds a predetermined level
US3979717A (en) * 1974-06-03 1976-09-07 United Technologies Corporation Helicopter warning system
US3947809A (en) * 1975-01-13 1976-03-30 Sundstrand Data Control, Inc. Below glide slope advisory warning system for aircraft
US4354237A (en) * 1980-06-24 1982-10-12 The Boeing Company Method and apparatus for producing an aircraft flare path control signal
US4490793A (en) * 1981-12-21 1984-12-25 Sperry Corporation Cruise speed control for aircraft performance management system
US4956780A (en) * 1988-12-08 1990-09-11 The Boeing Company Flight path angle command flight control system for landing flare
US20040167685A1 (en) * 2003-02-24 2004-08-26 Ryan Dean E. Runway overrun monitor and method for monitoring runway overruns
US8831799B1 (en) 2013-04-04 2014-09-09 The Boeing Company Flight director flare guidance
US9595200B2 (en) 2015-02-09 2017-03-14 The Boeing Company System and method for providing guidance during a flare maneuver of an aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2701111A (en) * 1951-09-22 1955-02-01 Honeywell Regulator Co Cruise control apparatus
US2875965A (en) * 1954-06-18 1959-03-03 Collins Radio Co Automatic flight control system
US2978210A (en) * 1955-10-28 1961-04-04 Honeywell Regulator Co Automatic pilots
US2953327A (en) * 1955-12-29 1960-09-20 Sperry Rand Corp Stall prevention system for aircraft
US3265333A (en) * 1964-02-03 1966-08-09 North American Aviation Inc Override control means for automatic landing system

Also Published As

Publication number Publication date
GB1178673A (en) 1970-01-21
US3489378A (en) 1970-01-13

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