FR1339114A - Moyens de commande automatique pour avion - Google Patents

Moyens de commande automatique pour avion

Info

Publication number
FR1339114A
FR1339114A FR913887A FR913887A FR1339114A FR 1339114 A FR1339114 A FR 1339114A FR 913887 A FR913887 A FR 913887A FR 913887 A FR913887 A FR 913887A FR 1339114 A FR1339114 A FR 1339114A
Authority
FR
France
Prior art keywords
aircraft
control means
automatic control
automatic
control
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
FR913887A
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.)
Lear Siegler Inc
Original Assignee
Lear Siegler Inc
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 Lear Siegler Inc filed Critical Lear Siegler Inc
Application granted granted Critical
Publication of FR1339114A publication Critical patent/FR1339114A/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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft

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)
FR913887A 1961-10-30 1962-10-30 Moyens de commande automatique pour avion Expired FR1339114A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US148630A US3275268A (en) 1961-10-30 1961-10-30 Automatic control for aircraft

Publications (1)

Publication Number Publication Date
FR1339114A true FR1339114A (fr) 1963-10-04

Family

ID=22526613

Family Applications (1)

Application Number Title Priority Date Filing Date
FR913887A Expired FR1339114A (fr) 1961-10-30 1962-10-30 Moyens de commande automatique pour avion

Country Status (2)

Country Link
US (1) US3275268A (fr)
FR (1) FR1339114A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2339920A1 (fr) * 1976-01-29 1977-08-26 Sperry Rand Corp Systeme de commande de stabilite selon l'axe des lacets pour engin aerien

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3988659A (en) * 1966-02-23 1976-10-26 Lear Siegler, Inc. Meridian seeking instrument
US3809867A (en) * 1972-12-18 1974-05-07 Collins Radio Co Synthesis of bank and pitch signals utilizing rate and acceleration input parameters
US3777242A (en) * 1972-12-21 1973-12-04 Collins Radio Co Turn coordination control with dead space and limited washout
US4935682A (en) * 1988-08-11 1990-06-19 The Boeing Company Full authority engine-out control augmentation subsystem

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2827250A (en) * 1954-02-11 1958-03-18 Honeywell Regulator Co Automatic pilots for aircraft
US2896883A (en) * 1955-01-12 1959-07-28 Sperry Rand Corp Aircraft automatic pilot
US2869804A (en) * 1955-07-26 1959-01-20 Hughes Aircraft Co Acceleration responsive control surface control limiting system for aircraft
US2936136A (en) * 1956-02-24 1960-05-10 Sperry Gyroscope Co Ltd Control systems for aircraft
US3071335A (en) * 1958-10-03 1963-01-01 United Aircraft Corp Flight control system
US3035795A (en) * 1959-11-27 1962-05-22 Honeywell Regulator Co Control apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2339920A1 (fr) * 1976-01-29 1977-08-26 Sperry Rand Corp Systeme de commande de stabilite selon l'axe des lacets pour engin aerien

Also Published As

Publication number Publication date
US3275268A (en) 1966-09-27

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