# US 11,908,329 B2 · Unusual attitude recovery symbology > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 11,908,329 B2 - Document ID: US11908329B2 - Status: Granted - Kind: B2 - Application number: 17/212,504 - Filed: 2021-03-25 - Published: 2022-09-29 - Granted: 2024-02-20 - Earliest claimed: 2021-03-25 - Assignees: Rockwell Collins, Inc. - Applicants: Rockwell Collins, Inc. - Inventors: Lenard E Noice - Web page: https://patentgrep.com/patent/US11908329B2 ## CPC - G01C 23/00: Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration - G08G 5/20: Arrangements for acquiring, generating, sharing or displaying traffic information (arrangements for monitoring traffic G08G5/72) - G08G 5/21: located onboard the aircraft - G08G 5/53: for cruising - G08G 5/55: for a single aircraft - G01C: MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY (measuring liquid level G01F; radio navigation, determining distance or velocity by use of propagation effects, e.g. Doppler effects, propagation time, of radio waves, analogous arrangements using other waves G01S) - G08G: TRAFFIC CONTROL SYSTEMS (guiding railway traffic, ensuring the safety of railway traffic B61L; arrangement of road signs or traffic signals E01F9/00; radar or analogous systems, sonar systems, lidar systems specially adapted for traffic control G01S13/91, G01S15/88, G01S17/88; {radar or analogous systems, sonar systems, lidar systems specially adapted for anti-collision purposes G01S13/93, G01S15/93, G01S17/93}) ## Abstract A system and related methods for providing unusual attitude symbology for recovering from an unusual attitude condition. By the unusual attitude symbology, a pilot may visually determine corrective actions needed to recover from the unusual attitude condition with a minimal recovery time and similarly with a minimal cognitive workload. The pilot may thus establish stable flight, even under a high-stress situation. The unusual attitude symbology includes pitch direction indicators, roll direction indicators, a roll recovery arc, an unusual attitude warning indicator, and a roll entry chevron. Path based symbology may also be used to provide unusual attitude recovery while maintaining spatial orientation of the aircraft to the outside scene. ## Claims ### Claim 1 A system for providing unusual attitude recovery symbology, comprising: at least one avionics display element configured to display an image associated with an aircraft, the image including at least: a roll scale; a roll pointer symbol configured to move about the roll scale, the roll pointer symbol representative of a current roll of the aircraft; and a flight path vector; and a boresight symbol; and at least one controller coupled to the avionics display element, the controller including at least one processor configured to: determine an entry of the aircraft into an unusual attitude condition, the unusual attitude condition including an unusual roll condition based on a roll of the aircraft; and update the image in response to determining the entry of the aircraft to the unusual attitude condition, the updated image further comprising unusual attitude symbology displayed relative to the roll scale, the unusual attitude symbology comprising: an unusual attitude warning indicator; and a roll recovery arc presenting a range of roll angles on the roll scale at which the aircraft may recover from the unusual roll condition, such that the unusual roll condition may be recovered from by positioning the roll pointer symbol within the range of roll angles on the roll scale; wherein the controller is further configured to update the image with a roll error tape, the roll error tape including at least one arc extending from one or more tips of the flight path vector, the at least one arc representative of a direction in which to roll the aircraft to correct for the unusual roll condition. ### Claim 2 (depends on 1) The system of claim 1, wherein prior to updating the image in response to determining the entry of the aircraft to the unusual attitude condition, the image further comprises at least one roll entry chevron on the roll scale, the roll entry chevron indicative of a roll of the aircraft at which the unusual roll condition is entered. ### Claim 3 (depends on 1) The system of claim 1, wherein the controller is further configured to: determine a recovery of the aircraft from the unusual roll condition; and update the image by removing at least the roll recovery arc in response to determining the recovery of the aircraft from the unusual roll condition. ### Claim 4 (depends on 3) The system of claim 3, wherein the roll recovery arc is removed from the image after a pre-determined delay. ### Claim 5 (depends on 1) The system of claim 1, wherein a video is maintained conformal with the image on the avionics display element during the unusual attitude condition. ### Claim 6 (depends on 1) The system of claim 1, wherein the unusual attitude condition further comprises an unusual pitch condition based on a pitch of the aircraft, wherein the unusual attitude symbology displayed relative to the roll scale further comprises a pitch direction indicator pointing in a direction in which to pitch the aircraft to recover from the unusual pitch condition. ### Claim 7 (depends on 6) The system of claim 6, wherein the pitch direction indicator is a shape indicative of a direction in which to pitch the aircraft to correct the unusual pitch condition; wherein the pitch direction indicator is fixed relative to the roll scale. ### Claim 8 (depends on 1) The system of claim 1, wherein the controller is further configured to update the image with a roll direction indicator, the roll direction indicator pointing in a direction in which to roll the aircraft to recover from the unusual roll condition. ### Claim 9 A system for providing unusual attitude recovery symbology, comprising: at least one avionics display element configured to display an image associated with an aircraft, the image including at least: a roll scale; roll pointer symbol configured to move about the roll scale, the roll pointer symbol representative of a current roll of the aircraft; a flight path vector; and a boresight symbol; and at least one controller coupled to the avionics display element, the controller including at least one processor configured to: determine an entry of the aircraft into an unusual attitude condition, the unusual attitude condition including an unusual roll condition based on a roll of the aircraft, the unusual attitude condition including an unusual pitch condition based on a pitch of the aircraft; update the image in response to determining the entry of the unusual attitude condition, the updated image further comprising unusual attitude recovery symbology displayed relative to the flight path vector, the unusual attitude recovery symbology comprising: a pitch direction indicator pointing in a direction in which to pitch the aircraft; and a roll direction indicator pointing in a direction in which to roll the aircraft; wherein upon determining the entry of the aircraft into the unusual attitude condition, the image is further updated with: a flight director guidance cue including a pitch reference point indicative of the pitch of the aircraft and one or more arms indicative of the roll of the aircraft; a pitch guide configured to indicate a pitch at which the aircraft may recover from the unusual pitch condition; and a roll guide configured to indicate a range of roll angles at which the aircraft may recover from the unusual roll condition; wherein the one or more arms extend to the roll guide; wherein the roll guide remains fixed relative to the flight director guidance cue. ### Claim 10 (depends on 9) The system of claim 9, wherein prior to updating the image in response to determining the entry of the aircraft to the unusual attitude condition, the image further comprises at least one roll entry chevron on the roll scale, the roll entry chevron indicative of a roll of the aircraft at which the unusual roll condition is entered. ### Claim 11 (depends on 9) The system of claim 9, wherein the controller is configured to: determine a recovery of the aircraft from the unusual roll condition; and update the image by removing at least the roll direction indicator in response to determining the recovery of the aircraft from the unusual roll condition. ### Claim 12 (depends on 11) The system of claim 11, wherein the controller is configured to: determine a recovery of the aircraft from the unusual pitch condition; and update the image by removing at least the pitch direction indicator in response to determining the recovery of the aircraft from the unusual roll condition. ### Claim 13 (depends on 9) The system of claim 9, wherein during the unusual roll condition, the flight director is emphasized, the emphasis including at least one of a color or a shape fill. ### Claim 14 (depends on 9) The system of claim 9, wherein the pitch direction indicator is a shape indicative of the direction in which to pitch the aircraft.