# US 12,759,696 B2 · Flight control system > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 12,759,696 B2 - Document ID: US12759696B2 - Status: Granted - Kind: B2 - Application number: 19/097,037 - Filed: 2025-04-01 - Published: 2025-10-09 - Granted: 2026-10-13 - Earliest claimed: 2024-04-08 - Assignees: Ratier-Figeac SAS - Applicants: Ratier-Figeac SAS - Inventors: Cedric Antraygue - Web page: https://patentgrep.com/patent/US12759696B2 ## CPC - B64C 13/0421: {control sticks for primary flight controls} - B64C: AEROPLANES; HELICOPTERS ## Abstract A flight control system for an aircraft. The aircraft has a set of principle axes including a roll axis and a pitch axis. The flight control system includes a control stick that is configured to move forwards and backwards and left and right to control movement of the aircraft about its roll and pitch axes, such movement of the control stick thus providing a first set of inputs to the flight control system. The control stick includes a further input in the form of a moveable element that can be moved between a range of positions and that is configured to provide a graduated input to the flight control system based on the position of the moveable element relative to a default position of the moveable element, the moveable element being positioned on a side or front portion of the control stick. ## Claims ### Claim 1 A flight control system for an aircraft, the aircraft having a set of principle axes including a roll axis and a pitch axis, the flight control system comprising: a control stick that is configured to move forwards and backwards and left and right to control movement of the aircraft about its roll and pitch axes, such movement of the control stick thus providing a first set of inputs to the flight control system, the control stick comprising a further input in the form of a moveable element that can be moved between a range of positions and that is configured to provide a graduated input to the flight control system based on the position of the moveable element relative to a default position of the moveable element, the moveable element being positioned on a side or front portion of the control stick and configured to rotate about an axis that is parallel to a central axis of the control stick. ### Claim 2 (depends on 1) The flight control system of claim 1, wherein the further input is configured to control movement of the aircraft about its yaw axis based on the position of the moveable element. ### Claim 3 (depends on 2) The flight control system of claim 2, wherein the further input is configured to control movement of the aircraft about its yaw axis during flight and also to control steering of the aircraft when taxiing. ### Claim 4 (depends on 1) The flight control system of claim 1, wherein the moveable element comprises a finger-operated stick, finger-operated lever, finger-operated roller, or finger-operated slider, that can be moved relative to the rest of the control stick to control the further input to the flight control system. ### Claim 5 (depends on 1) The flight control system of claim 1, wherein the moveable element is configured to move forwards and backwards relative to the rest of the control stick or wherein the moveable element is configured to move left and right relative to the rest of the control stick. ### Claim 6 (depends on 1) The flight control system of claim 1, wherein the moveable element is configured to be continuously moved between the range of positions, the range of positions extending either side of the default position of the moveable element. ### Claim 7 (depends on 1) The flight control system of claim 1, wherein the control stick has a total length extending from a bottom end to a top end, the moveable element being spaced from the top end by a distance that is at least 5% of the total length of the control stick or being spaced from the bottom end of the control stick by a distance that is at least 40% of the total length of the control stick. ### Claim 8 (depends on 1) The flight control system of claim 1, wherein the control stick further comprises a second moveable element provided on an upper surface of the control stick to provide a yet further input to the flight control system. ### Claim 9 (depends on 8) The flight control system of claim 8, wherein the flight control system is configured such that the second moveable element controls braking of the aircraft. ### Claim 10 (depends on 1) The flight control system of claim 1, wherein the control stick is constrained to move forwards and backwards and right and left such that twisting movement of the control stick is prevented. ### Claim 11 A control stick for use with the flight control system for an aircraft, the aircraft having a set of principle axes including a roll axis and a pitch axis, wherein the control stick is configured to move forward and backwards and left and right to provide a first set of inputs, the control stick comprising: a moveable element configured to provide a further input, the moveable element being continuously moveable between a range of positions, the moveable element being positioned on a side of the control stick and configured to rotate about an axis that is parallel to a central axis of the control stick. ### Claim 12 (depends on 11) The control stick of claim 11, wherein the moveable element is configured to move in a circumferential direction relative to a central axis of the control stick. ### Claim 13 (depends on 11) The control stick of claim 11, wherein the moveable element comprises a finger-operated stick, finger-operated lever, finger-operated roller, or finger-operated slider, that can be moved relative to the control stick to control the further input. ### Claim 14 (depends on 11) The control stick of claim 11, wherein the control stick further comprises a second moveable element provided on an upper surface of the control stick to provide a yet further input.