GB1497182A - System for controlling the position of the anchorage point of the piloting channel of an aircraft - Google Patents

System for controlling the position of the anchorage point of the piloting channel of an aircraft

Info

Publication number
GB1497182A
GB1497182A GB22842/75A GB2284275A GB1497182A GB 1497182 A GB1497182 A GB 1497182A GB 22842/75 A GB22842/75 A GB 22842/75A GB 2284275 A GB2284275 A GB 2284275A GB 1497182 A GB1497182 A GB 1497182A
Authority
GB
United Kingdom
Prior art keywords
control
aircraft
piloting
manual
action
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
GB22842/75A
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of GB1497182A publication Critical patent/GB1497182A/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
    • G05D1/08—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
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0833—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using limited authority control
    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa

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)
  • Computer Security & Cryptography (AREA)
  • Toys (AREA)
  • Control Of Multiple Motors (AREA)
  • Control Of Position Or Direction (AREA)
  • Mechanical Control Devices (AREA)
GB22842/75A 1974-06-06 1975-05-23 System for controlling the position of the anchorage point of the piloting channel of an aircraft Expired GB1497182A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7419532A FR2273709A1 (fr) 1974-06-06 1974-06-06 Dispositif de commande de la position du point d'ancrage d'une chaine de pilotage d'un aerodyne

Publications (1)

Publication Number Publication Date
GB1497182A true GB1497182A (en) 1978-01-05

Family

ID=9139697

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22842/75A Expired GB1497182A (en) 1974-06-06 1975-05-23 System for controlling the position of the anchorage point of the piloting channel of an aircraft

Country Status (4)

Country Link
US (1) US3981461A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE2524318C3 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2273709A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1497182A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB803574A (en) * 1954-08-25 1958-10-29 Sperry Gyroscope Co Ltd Control systems for aircraft
US3051418A (en) * 1960-09-27 1962-08-28 Boeing Co Flight control system
US3584814A (en) * 1967-07-18 1971-06-15 Bell Aerospace Corp Stability and control augmentation system
GB1202778A (en) * 1968-02-06 1970-08-19 Ferranti Ltd Improvements relating to flight aid systems
FR2137300B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1971-05-18 1974-04-05 Aerospatiale

Also Published As

Publication number Publication date
FR2273709B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1976-10-15
FR2273709A1 (fr) 1976-01-02
US3981461A (en) 1976-09-21
DE2524318C3 (de) 1980-11-13
DE2524318A1 (de) 1975-12-18
DE2524318B2 (de) 1980-03-20

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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