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GB2618154B - A control unit in an active inceptor - Google Patents

A control unit in an active inceptor Download PDF

Info

Publication number
GB2618154B
GB2618154B GB2206340.8A GB202206340A GB2618154B GB 2618154 B GB2618154 B GB 2618154B GB 202206340 A GB202206340 A GB 202206340A GB 2618154 B GB2618154 B GB 2618154B
Authority
GB
United Kingdom
Prior art keywords
control unit
active inceptor
inceptor
active
unit
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
GB2206340.8A
Other versions
GB202206340D0 (en
GB2618154A (en
Inventor
Mark Dee Justin
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 GB2206340.8A priority Critical patent/GB2618154B/en
Publication of GB202206340D0 publication Critical patent/GB202206340D0/en
Priority to US18/860,161 priority patent/US20250293626A1/en
Priority to EP23719059.0A priority patent/EP4514682A1/en
Priority to JP2024563582A priority patent/JP2025514973A/en
Priority to PCT/GB2023/051033 priority patent/WO2023209335A1/en
Priority to TW112115349A priority patent/TW202408880A/en
Publication of GB2618154A publication Critical patent/GB2618154A/en
Application granted granted Critical
Publication of GB2618154B publication Critical patent/GB2618154B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
    • B64C13/507Transmitting means with power amplification using electrical energy with artificial feel
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05GCONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G9/00Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
    • G05G9/02Manually-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
    • G05G9/04Manually-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
    • G05G9/047Manually-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
    • G05G2009/04766Manually-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 providing feel, e.g. indexing means, means to create counterforce
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05GCONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G5/00Means for preventing, limiting or returning the movements of parts of a control mechanism, e.g. locking controlling member
    • G05G5/03Means for enhancing the operator's awareness of arrival of the controlling member at a command or datum position; Providing feel, e.g. means for creating a counterforce
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05GCONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G9/00Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
    • G05G9/02Manually-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
    • G05G9/04Manually-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
    • G05G9/047Manually-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)
  • Control Of Electric Motors In General (AREA)
GB2206340.8A 2022-04-29 2022-04-29 A control unit in an active inceptor Active GB2618154B (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB2206340.8A GB2618154B (en) 2022-04-29 2022-04-29 A control unit in an active inceptor
PCT/GB2023/051033 WO2023209335A1 (en) 2022-04-29 2023-04-20 A control unit in an active inceptor
EP23719059.0A EP4514682A1 (en) 2022-04-29 2023-04-20 A control unit in an active inceptor
JP2024563582A JP2025514973A (en) 2022-04-29 2023-04-20 Control unit in the active interceptor
US18/860,161 US20250293626A1 (en) 2022-04-29 2023-04-20 Control unit in an active inceptor
TW112115349A TW202408880A (en) 2022-04-29 2023-04-25 A control unit in an active inceptor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2206340.8A GB2618154B (en) 2022-04-29 2022-04-29 A control unit in an active inceptor

Publications (3)

Publication Number Publication Date
GB202206340D0 GB202206340D0 (en) 2022-06-15
GB2618154A GB2618154A (en) 2023-11-01
GB2618154B true GB2618154B (en) 2025-01-22

Family

ID=81943764

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2206340.8A Active GB2618154B (en) 2022-04-29 2022-04-29 A control unit in an active inceptor

Country Status (1)

Country Link
GB (1) GB2618154B (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080156939A1 (en) * 2007-01-03 2008-07-03 Honeywell International, Inc. Active pilot flight control stick system with passive electromagnetic feedback
GB2482407A (en) * 2010-07-28 2012-02-01 Woodward Mpc Inc Position control system for cross coupled operation of fly-by-wire control columns
US20120056039A1 (en) * 2010-08-30 2012-03-08 Liebherr-Aerospace Lindenberg Gmbh Control system for an aircraft

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080156939A1 (en) * 2007-01-03 2008-07-03 Honeywell International, Inc. Active pilot flight control stick system with passive electromagnetic feedback
GB2482407A (en) * 2010-07-28 2012-02-01 Woodward Mpc Inc Position control system for cross coupled operation of fly-by-wire control columns
US20120056039A1 (en) * 2010-08-30 2012-03-08 Liebherr-Aerospace Lindenberg Gmbh Control system for an aircraft

Also Published As

Publication number Publication date
GB202206340D0 (en) 2022-06-15
GB2618154A (en) 2023-11-01

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