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GB2569601B - Aircraft control systems - Google Patents

Aircraft control systems Download PDF

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Publication number
GB2569601B
GB2569601B GB1721529.4A GB201721529A GB2569601B GB 2569601 B GB2569601 B GB 2569601B GB 201721529 A GB201721529 A GB 201721529A GB 2569601 B GB2569601 B GB 2569601B
Authority
GB
United Kingdom
Prior art keywords
control systems
aircraft control
aircraft
systems
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.)
Active
Application number
GB1721529.4A
Other versions
GB2569601A (en
GB201721529D0 (en
Inventor
Taylor Adam
David Draper Jonathan
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.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
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 BAE Systems PLC filed Critical BAE Systems PLC
Priority to GB1721529.4A priority Critical patent/GB2569601B/en
Publication of GB201721529D0 publication Critical patent/GB201721529D0/en
Priority to JP2020534188A priority patent/JP7005770B2/en
Priority to MA051273A priority patent/MA51273A/en
Priority to US16/771,315 priority patent/US11174005B2/en
Priority to KR1020207018166A priority patent/KR102650037B1/en
Priority to PCT/GB2018/053448 priority patent/WO2019122807A1/en
Priority to CN201880082281.6A priority patent/CN111556841B/en
Priority to EP18811338.5A priority patent/EP3728026B1/en
Priority to CA3085054A priority patent/CA3085054A1/en
Priority to ES18811338T priority patent/ES2949956T3/en
Publication of GB2569601A publication Critical patent/GB2569601A/en
Application granted granted Critical
Publication of GB2569601B publication Critical patent/GB2569601B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/503—Fly-by-Wire
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G9/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
    • G05G9/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only
    • G05G9/04—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously
    • G05G9/047—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously the controlling member being movable by hand about orthogonal axes, e.g. joysticks

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Control Devices (AREA)
GB1721529.4A 2017-12-21 2017-12-21 Aircraft control systems Active GB2569601B (en)

Priority Applications (10)

Application Number Priority Date Filing Date Title
GB1721529.4A GB2569601B (en) 2017-12-21 2017-12-21 Aircraft control systems
CA3085054A CA3085054A1 (en) 2017-12-21 2018-11-29 Aircraft control systems
JP2020534188A JP7005770B2 (en) 2017-12-21 2018-11-29 Aircraft control system
US16/771,315 US11174005B2 (en) 2017-12-21 2018-11-29 Aircraft control systems
KR1020207018166A KR102650037B1 (en) 2017-12-21 2018-11-29 aircraft control system
PCT/GB2018/053448 WO2019122807A1 (en) 2017-12-21 2018-11-29 Aircraft control systems
CN201880082281.6A CN111556841B (en) 2017-12-21 2018-11-29 Aircraft control system
EP18811338.5A EP3728026B1 (en) 2017-12-21 2018-11-29 Aircraft control systems
MA051273A MA51273A (en) 2017-12-21 2018-11-29 AIRCRAFT CONTROL SYSTEMS
ES18811338T ES2949956T3 (en) 2017-12-21 2018-11-29 Aircraft control systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1721529.4A GB2569601B (en) 2017-12-21 2017-12-21 Aircraft control systems

Publications (3)

Publication Number Publication Date
GB201721529D0 GB201721529D0 (en) 2018-02-07
GB2569601A GB2569601A (en) 2019-06-26
GB2569601B true GB2569601B (en) 2022-05-11

Family

ID=61131458

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1721529.4A Active GB2569601B (en) 2017-12-21 2017-12-21 Aircraft control systems

Country Status (1)

Country Link
GB (1) GB2569601B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2589059B (en) 2019-09-17 2024-05-15 Bae Systems Plc Taxiing method and apparatus

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4188834A (en) * 1976-06-08 1980-02-19 Honda Giken Kogyo Kabushiki Kaisha Operating device
EP2072395A2 (en) * 2007-12-17 2009-06-24 Honeywell International Inc. Limited authority and full authority mode fly-by-wire flight control surface actuation control system
US20090187292A1 (en) * 2008-01-17 2009-07-23 Mark Andrew Hreha Integrated pitch, roll, and yaw inceptor
GB2471213A (en) * 2006-08-29 2010-12-22 Borealis Tech Ltd Method for controlling aircraft nosewheels
US20130138274A1 (en) * 2011-11-28 2013-05-30 Embraer S.A. Flight Control System Mode And Method Providing Aircraft Speed Control Through The Usage Of Momentary On-Off Control

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4188834A (en) * 1976-06-08 1980-02-19 Honda Giken Kogyo Kabushiki Kaisha Operating device
GB2471213A (en) * 2006-08-29 2010-12-22 Borealis Tech Ltd Method for controlling aircraft nosewheels
EP2072395A2 (en) * 2007-12-17 2009-06-24 Honeywell International Inc. Limited authority and full authority mode fly-by-wire flight control surface actuation control system
US20090187292A1 (en) * 2008-01-17 2009-07-23 Mark Andrew Hreha Integrated pitch, roll, and yaw inceptor
US20130138274A1 (en) * 2011-11-28 2013-05-30 Embraer S.A. Flight Control System Mode And Method Providing Aircraft Speed Control Through The Usage Of Momentary On-Off Control

Also Published As

Publication number Publication date
GB2569601A (en) 2019-06-26
GB201721529D0 (en) 2018-02-07

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