GB2569601B - Aircraft control systems - Google Patents
Aircraft control systems Download PDFInfo
- 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
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)
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1721529.4A GB2569601B (en) | 2017-12-21 | 2017-12-21 | Aircraft control systems |
EP18811338.5A EP3728026B1 (en) | 2017-12-21 | 2018-11-29 | Aircraft control systems |
US16/771,315 US11174005B2 (en) | 2017-12-21 | 2018-11-29 | Aircraft control systems |
CN201880082281.6A CN111556841A (en) | 2017-12-21 | 2018-11-29 | Aircraft control system |
KR1020207018166A KR102650037B1 (en) | 2017-12-21 | 2018-11-29 | aircraft control system |
JP2020534188A JP7005770B2 (en) | 2017-12-21 | 2018-11-29 | Aircraft control system |
PCT/GB2018/053448 WO2019122807A1 (en) | 2017-12-21 | 2018-11-29 | Aircraft control systems |
ES18811338T ES2949956T3 (en) | 2017-12-21 | 2018-11-29 | Aircraft control systems |
MA051273A MA51273A (en) | 2017-12-21 | 2018-11-29 | AIRCRAFT CONTROL SYSTEMS |
CA3085054A CA3085054A1 (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)
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)
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 |
-
2017
- 2017-12-21 GB GB1721529.4A patent/GB2569601B/en active Active
Patent Citations (5)
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 |
---|---|
GB201721529D0 (en) | 2018-02-07 |
GB2569601A (en) | 2019-06-26 |
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