Time varying loudness prediction system

US11900818B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11900818-B2
Application numberUS-202016897699-A
CountryUS
Kind codeB2
Filing dateJun 10, 2020
Priority dateJun 10, 2019
Publication dateFeb 13, 2024
Grant dateFeb 13, 2024

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Abstract

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Disclosed are methods and systems for predicting time varying loudness in a geographic region. Training data, including noise information, weather information, and traffic information is collected from a plurality of sensors located in a plurality of geographic regions. The information is collected during multiple time periods. The noise information includes time varying loudness. Static features of the geographic regions are also defined and included in the training data. The static and time varying dynamic features train a model. The model is used predict time varying loudness within a different region and at a time later than times the training data is collected. The predicted loudness levels are utilized, in some aspects, to determine a route for an aircraft.

First claim

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We claim: 1. A system, comprising: hardware processing circuitry; one or more hardware memories storing instructions that when executed configure the hardware processing circuitry to perform operations comprising: receiving measurements of dynamic feature data for a geographic region; determining static features for the geographic region; generating a predicted background noise loudness in the geographic region during a defined time period using a model, the model trained on training data including historical measurements of dynamic feature data for a plurality of regions over a plurality of training time periods and static features of the plurality of regions, wherein the geographic region is absent from the plurality of regions, wherein the defined time period occurs after the plurality, of training time periods; determining, based on the predicted background noise loudness, whether to route an aircraft through the geographic region; determining a route and one or more operating constraints based on the predicted background noise loudness in the geographic region, the one or more operating constraints indicative of at least one of: a take-off maneuver or a landing maneuver associated with the route; selecting an aircraft, from among a plurality of different aircrafts, for the route based on the predicted background noise loudness, the one or more operating constraints, and capabilities of the aircraft; and routing the aircraft through a particular geographic region based on the determined route. 2. The system of claim 1 , wherein the generating of the predicted background noise loudness predicts the background noise loudness at a particular time of day and a particular date within the defined time period, and the historical measurements of the dynamic feature data are correlated with a time of day and a date of the historical measurements. 3. The system of claim 1 , the operations further comprising: wherein generating the predicted background noise loudness comprises: predicting a first background noise loudness in a first region during the defined time period based on the model; predicting a second background noise loudness in a second region during the defined time period based on the model; determining the first background noise loudness is higher than the second background noise loudness; and wherein routing the aircraft comprises routing the aircraft through the first region during the defined time period in response to the determination. 4. The system of claim 1 , the operations further comprising: wherein generating the predicted background noise loudness comprises generating, based on the model and for each of the plurality of regions in a map, a predicted background noise loudness of the respective region; wherein determining the route comprises: identifying an origin and destination; identifying a plurality of routes from the origin to the destination, each of the plurality of routes including at least one of the plurality of regions in the map; determining a comparison of the predicted background noise loudness of the at least one of the plurality of regions included in a first route of the plurality of routes to the predicted background noise loudness of the at least one of the plurality of regions included in a second route of the plurality of routes; and selecting the first route or the second route based on the comparison; and wherein routing the aircraft comprises routing the aircraft over the selected route. 5. The system of claim 4 , the operations further comprising: aggregating predicted background noise loudness of regions included in the first route; and aggregating predicted background noise loudness of regions included in the second route, wherein the selection of the first route or the second route is based on the first route aggregating and the second route aggregating. 6. The system of claim 4 , the operations further comprising: determining a minimum predicted background noise loudness along the selected route; comparing the minimum predicted background noise loudness to a noise threshold; and determining an altitude for the aircraft, along the selected route to be above a predefined altitude in response to the minimum predicted background noise loudness being below the noise threshold. 7. The system of claim 1 , wherein the capabilities of the aircraft are indicative of the ability of the aircraft to perform one or more maneuvers for the route and complete the route without violating a noise threshold given the predicted background noise loudness. 8. The system of claim 1 , wherein the take-off maneuver comprises a take-off angle and the landing maneuver comprises a landing angle. 9. A non-transitory computer readable storage medium comprising instructions that when executed configure hardware processing circuitry to perform operations comprising: receiving measurements of dynamic feature data for a geographic region; determining static features for the geographic region; and generating a predicted background noise loudness in the geographic region during a defined time period using a model, the model trained on training data including historical measurements of dynamic feature data for a plurality of regions over a plurality of training time periods and static features of the plurality of regions, wherein the geographic region is absent from the plurality of regions, wherein the defined time period occurs after the plurality of training time periods; determining, based on the predicted background noise loudness, whether to route an aircraft through the geographic region; determining a route and one or more operating constraints based on the predicted background noise loudness in the geographic region, the one or more operating constraints indicative of at least one of: a take-off maneuver or a landing maneuver associated with the route; selecting an aircraft, from among a plurality of different aircrafts, for the route based on the predicted background noise loudness, the one or more operating constraints, and capabilities of the aircraft; and routing the aircraft through the geographic region based on the determined route. 10. The non-transitory computer readable storage medium of claim 9 , the operations further comprising: wherein generating the predicted background noise loudness comprises: predicting a first background noise loudness in a first region during the defined time period based on the model; predicting a second background noise loudness in a second region during the defined time period based on the model; determining the first background noise loudness is higher than the second background noise loudness; and wherein routing the aircraft comprises routing the aircraft through the first region during the defined time period in response to the determination. 11. The non-transitory computer readable storage medium of claim 9 , the operations further comprising: wherein generating the predicted background noise loudness comprises generating, based on the model and for each of the plurality of regions in a map, a predicted background noise loudness of the respective region; wherein determining the route comprises: identifying an origin and destination of an aircraft; identifying a plurality of routes from the origin to the destination, each of the plurality of routes including at least one of the plurality of regions in the map; determining a comparison of the predicted background noise loudness of the at least one of the plurality of regions included in a first route of the plurality of routes to the predicted background noise loudness of the at least one of the plurality of regions included in

Assignees

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Classifications

  • Supervised learning · CPC title

  • for a single aircraft · CPC title

  • Navigation or guidance aids · CPC title

  • Transmission of traffic-related information between aircraft and ground stations · CPC title

  • Traffic control systems for aircraft · CPC title

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Frequently asked questions

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What does patent US11900818B2 cover?
Disclosed are methods and systems for predicting time varying loudness in a geographic region. Training data, including noise information, weather information, and traffic information is collected from a plurality of sensors located in a plurality of geographic regions. The information is collected during multiple time periods. The noise information includes time varying loudness. Static featur…
Who is the assignee on this patent?
Joby Aero Inc
What technology area does this patent fall under?
Primary CPC classification G08G5/32. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Feb 13 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).