Static inverse desymmetrized propellers
First Claim
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1. A computer-implemented method, comprising:
- receiving, by a computer system, input that identifies a sound spectrum, the input identified by a user, the sound spectrum comprising at least one of frequency, amplitude, or phase;
generating, by the computer system, a sound profile for the user based in part on the input, the sound profile identifying at least one of a loudness, roughness, sharpness, fluctuation strength, or tonal prominence associated with the sound of the input;
identifying, by the computer system, components of an unmanned aerial vehicle (UAV) for determining one or more acoustic models of the UAV based in part on the sound profile;
ranking, by the computer system, the components based in part on the sound profile;
generating, by the computer system, a particular acoustic model based in part on the ranked components that are associated with the UAV;
identifying, by the computer system, the particular acoustic model of an expected UAV configuration that corresponds to the sound profile; and
instructing, by the computer system, manufacture of the UAV using the configuration identified by the particular acoustic model.
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Abstract
Techniques for using a sound spectrum to generate models, which identify unmanned aerial vehicle (UAV) configurations, are described herein. The models may be based on components associated with a UAV, and instructions for manufacture of a UAV may be provided. For example, a sound spectrum may be obtained by a computer system which is used to generate one or more models. The one or more models are based in part on components of a UAV and identify UAV configurations that will generate an expected sound within the identified sound spectrum. The UAV configurations identified by the models are used to instruct manufacture of a UAV.
35 Citations
19 Claims
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1. A computer-implemented method, comprising:
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receiving, by a computer system, input that identifies a sound spectrum, the input identified by a user, the sound spectrum comprising at least one of frequency, amplitude, or phase; generating, by the computer system, a sound profile for the user based in part on the input, the sound profile identifying at least one of a loudness, roughness, sharpness, fluctuation strength, or tonal prominence associated with the sound of the input; identifying, by the computer system, components of an unmanned aerial vehicle (UAV) for determining one or more acoustic models of the UAV based in part on the sound profile; ranking, by the computer system, the components based in part on the sound profile; generating, by the computer system, a particular acoustic model based in part on the ranked components that are associated with the UAV; identifying, by the computer system, the particular acoustic model of an expected UAV configuration that corresponds to the sound profile; and instructing, by the computer system, manufacture of the UAV using the configuration identified by the particular acoustic model. - View Dependent Claims (2, 3, 4, 18)
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5. A computer-implemented method, comprising:
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obtaining, by a computer system, a sound spectrum comprising at least one of frequency, amplitude, or phase; generating, by the computer system, one or more models based in part on one or more components that are associated with an unmanned aerial vehicle (UAV), a particular model of the one or more models identifying a particular UAV configuration that will generate an expected sound within a range of the sound spectrum, the expected sound associated with a sound profile that identifies at least one of a loudness, roughness, sharpness, fluctuation strength, or tonal prominence associated with the expected sound; and instructing, by the computer system, manufacture of the UAV using the particular configuration identified by the model. - View Dependent Claims (6, 7, 8, 9, 10, 11, 12)
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13. A computer-implemented method, comprising:
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obtaining, by a computer system, a sound spectrum comprising at least one of frequency, amplitude, or phase; identifying, by the computer system, components of an unmanned aerial vehicle (UAV) for determining one or more acoustic models of the UAV based in part on the sound spectrum; and generating, by the computer system, a configuration of the components for the UAV based in part on an acoustic model of the one or more acoustic models, the configuration enabling the UAV to generate a sound corresponding to the sound spectrum, the sound associated with a sound profile that identifies at least one of a loudness, roughness, sharpness, fluctuation strength, or tonal prominence associated with the sound. - View Dependent Claims (14, 15, 16, 17, 19)
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Specification