초록 ▼

This disclosure is directed to an automated aerial vehicle (“AAV”) and systems, devices, and techniques pertaining to canceling noise, generating audible communications, and/or generating visible communications. The AAV may include one or more propellers utilized, in part, to produce sound that canc

This disclosure is directed to an automated aerial vehicle (“AAV”) and systems, devices, and techniques pertaining to canceling noise, generating audible communications, and/or generating visible communications. The AAV may include one or more propellers utilized, in part, to produce sound that cancels noise generated by one or more other propellers. Additionally or alternatively, the AAV may utilize one or more propellers to generate audible and/or visible communications.

대표청구항 ▼

1. An automated aerial vehicle (AAV) comprising: a plurality of propellers that include: a first propeller operable to rotate in a first rotational direction to cause lift of the AAV, the first propeller generating noise sound waves while rotating; anda second propeller operable to rotate in a secon

1. An automated aerial vehicle (AAV) comprising: a plurality of propellers that include: a first propeller operable to rotate in a first rotational direction to cause lift of the AAV, the first propeller generating noise sound waves while rotating; anda second propeller operable to rotate in a second rotational direction that is opposite the first rotational direction, the second propeller being located in a same plane as the first propeller and having a different axis of rotation than the first propeller;a microphone to detect the noise sound waves generated by at least the first propeller;a first propeller motor that drives rotation of the first propeller;a second propeller motor that drives rotation of the second propeller; anda control system in communication with at least the microphone, the first propeller, and the second propeller motor, the control system configured to: receive a signal representing the detected noise sound waves;cause the propeller motor to modulate rotational speed of the second propeller such that the second propeller generates anti-noise sound waves that are in antiphase with the noise sound waves generated by the first propeller and that have a same amplitude as the noise sound waves, the anti-noise sound waves substantially canceling the noise sound waves;detect that an object is in a flight path of the AAV;determine a plurality of rotational speed modulations that cause at least one propeller of the plurality of propellers to generate a series of sounds that correspond to an audible communication; andmodulate rotational speed of the at least one propeller based on the determined plurality of rotational speed modulations to communicate the audible communication. 2. The AAV of claim 1, further comprising a plurality of light-emitting diodes (LEDs), individual LEDs of the plurality of LEDs being coupled to a propeller of the plurality of propellers, the control system further configured to: determine that a person is in a flight path of the AAV;determine a series of LED illuminations that correspond to a visible communication, wherein determining the series of LED illuminations includes: determining a first LED of the plurality of LEDs to illuminate at a first time; anddetermining a second LED of the plurality of LEDs to illuminate at a second time, the second time being different than the first time; andcause illumination of the plurality of LEDs based on the determined series of LED illuminations to communicate the visible communication. 3. The AAV of claim 2, wherein the first LED is coupled to the first propeller of the plurality of propellers and the second LED is coupled to the second propeller of the plurality of propellers. 4. A vehicle comprising: a plurality of rotors that include: a first rotor operable to rotate about a first center of rotation and cause propulsion of the vehicle, the rotor generating noise while rotating; anda second rotor operable to rotate about a second center of rotation; anda control system configured to: receive a signal representing one or more operational characteristics of the first rotor;cause modulation of at least one of the second rotor or a sound generator to produce sound that substantially cancels the noise generated by the first rotor, the modulation being determined based at least in part on the received signal; andcause modulation of at least one of the plurality of rotors such that the at least one of the plurality of rotors generates an audible communication. 5. The vehicle of claim 4, wherein: the first rotor rotates in a first rotational direction; andthe second rotor rotates in a second rotational direction that is opposite the first rotational direction. 6. The vehicle of claim 4, further comprising an audio sensor that is configured to detect the noise generated by the first rotor, and wherein the control system is configured to receive a signal representing one or more operational characteristics of the first rotor comprises the control system being configured to receive, from the audio sensor, a signal representing the noise. 7. The vehicle of claim 4, wherein: the first rotor is operable to rotate in a first rotational direction;the second rotor is operable to rotate in a second rotational direction that is opposite the first rotational direction; andthe control system being configured to cause modulation of at least one of the second rotor or the sound generator comprises the control system being configured to cause modulation of rotational speed of the second rotor to modulate the sound produced by the second rotor. 8. The vehicle of claim 7, further comprising an audio sensor that is configured to detect the noise generated by the first rotor, and wherein the control system being configured to receive a signal representing one or more operational characteristics of the first rotor comprises the control system being configured to receive, from the audio sensor, a signal representing the detected noise. 9. The vehicle of claim 4, wherein the control system being configured to cause modulation of the sound generator comprises the control system being configured to cause modulation of the sound generator at a rate of modulation of approximately 10 kHz or higher. 10. The vehicle of claim 4, wherein the vehicle comprises an automated aerial vehicle (AAV). 11. The vehicle of claim 4, wherein the one or more operational characteristics of the first rotor includes rotational speed of the first rotor. 12. The vehicle of claim 4, wherein the sound generator comprises an audio speaker. 13. The vehicle of claim 4, further comprising a plurality of audio sensors configured to detect ambient sound outside the vehicle, wherein: a first audio sensor of the plurality of audio sensors is disposed proximate the first rotor of the plurality of rotors;a second audio sensor of the plurality of audio sensors is disposed proximate the second rotor of the plurality of rotors; andthe control system is further configured to cause modulation of the at least one of the plurality of rotors such that the at least one of the plurality of rotors generates the audible communication includes: receive a first signal from the first audio sensor, the first signal representing first detected ambient noise that includes noise generated by the first rotor;receive a second signal from the second audio sensor, the second signal representing second detected ambient noise that includes noise generated by the second rotor;determine a global ambient noise based at least in part on the first received signal and the second received signal;determine a plurality of modulations of rotational speed of one or more rotors of the plurality of rotors, the plurality of modulations corresponding to the audible communication; andcause modulation of rotational speed of the one or more rotors of the plurality of rotors based on the determined plurality of modulations such that the one or more rotors produce a series of sounds that provide the audible communication, the audible communication being perceptible from outside the vehicle. 14. A method comprising: detecting noise generated by a first propeller of a plurality of propellers of an aerial vehicle;modulating, based at least in part on the detected noise, rotational speed of a second propeller of the plurality of propellers of the aerial vehicle such that the second propeller produces sound that substantially cancels the noise generated by the first propeller, wherein the first propeller and the second propeller are located substantially in a same plane and have different axes of rotation; andilluminating at least a portion of one or more propellers of the plurality of propellers to produce a visible communication. 15. The method of claim 14, wherein the detecting noise comprises detecting, via a first audio sensor, first noise that is generated by the first propeller of the plurality of propellers, the method further comprising detecting, via a second audio sensor, second noise that is generated by a third propeller of the plurality of propellers. 16. The method of claim 15, further comprising: determining a global ambient noise based at least in part on the detected first noise and the detected second noise; andmodulating rotational speed of one or more propellers of the plurality of propellers based at least in part on the determined global ambient noise. 17. The method of claim 14, further comprising modulating rotational speed of one or more propellers of the plurality of propellers to cause the one or more propellers to produce a series of sounds corresponding to an audible communication. 18. The method of claim 14, wherein the illuminating at least the portion of the one or more propellers of the plurality of propellers to produce the visible communication comprises: illuminating at least a first portion of the first propeller at a first time; andilluminating at least a second portion of the second propeller at a second time. 19. The method of claim 18, wherein the second time is different than the first time. 20. The method of claim 14, wherein multiple light-emitting diodes (LEDs) are coupled to individual propellers of the plurality of propellers, and wherein the illuminating at least the portion of the one or more propellers of the plurality of propellers to produce the visible communication comprises: illuminating a first LED that is coupled to the first propeller of the plurality of propellers at a first time; andilluminating a second LED that is coupled to the second propeller of the plurality of propellers at a second time, the second time being different than the first time.