Systems and methods to calibrate spectral characteristics of imaging sensors

    公开(公告)号:US10812788B1

    公开(公告)日:2020-10-20

    申请号:US16436509

    申请日:2019-06-10

    Abstract: Systems and methods to calibrate an imaging sensor may include an enclosure with a controlled environment, a light source illuminating the environment, and a particle source emitting desired particles at desired concentrations into the environment. An imaging sensor, which may be associated with an aerial vehicle, may be placed within the enclosure, and the imaging sensor may capture imaging data within the controlled environment. In addition, the imaging data may be processed to determine current spectral characteristics of the imaging sensor. Based on the environment, light, and particle properties within the environment, the imaging sensor may be calibrated to exhibit nominal or desired spectral characteristics.

    Simulated flight data to determine delivery timeframes for aerial item delivery

    公开(公告)号:US10776744B1

    公开(公告)日:2020-09-15

    申请号:US15473481

    申请日:2017-03-29

    Abstract: Described are example systems and methods that utilize simulated and/or actual flight data to determine an aerial delivery time estimate between a source location and a delivery destination, based on current flight conditions. For example, multiple flight simulations along a flight path between a source location and a delivery destination may be performed based on various different flight conditions and the flight time determined from the simulations may be maintained in a data store, associated with the flight path and simulated flight conditions. When a request for item information is received, current flight conditions may be determined and used to determine an estimated flight time based on stored simulated flight data having similar flight conditions to the current flight conditions.

    Airlift package protection airbag container

    公开(公告)号:US10676192B1

    公开(公告)日:2020-06-09

    申请号:US16199754

    申请日:2018-11-26

    Abstract: An airbag container may be inflated and used to protect an item placed within the airbag container. The airbag container may include an inflatable portion that includes sidewalls that extend between a cover to a base. The airbag container may include an orifice to receive gas to inflate the sidewalls, the cover, and the base to an inflation pressure. The airbag container may include an inner cavity defined within the sidewalls, the cover, and the base. The inner cavity may be unpressurized when the inflatable body is at the inflation pressure. The cover may be at least partially separable from the sidewalls to enable insertion of an item in the inner cavity. The cover may then be securable to the sidewalls to securely contain the item in the inner cavity.

    RING WING AERIAL VEHICLE
    85.
    发明申请

    公开(公告)号:US20200094961A1

    公开(公告)日:2020-03-26

    申请号:US16682638

    申请日:2019-11-13

    Abstract: Described is an apparatus and method of an aerial vehicle, such as an unmanned aerial vehicle (“UAV”) that can operate in either a vertical takeoff and landing (VTOL) orientation or a horizontal flight orientation. The aerial vehicle includes a plurality of propulsion mechanisms that enable the aerial vehicle to move in any of the six degrees of freedom (surge, sway, heave, pitch, yaw, and roll) when in the VTOL orientation. The aerial vehicle also includes a ring wing that surrounds the propulsion mechanisms and provides lift to the aerial vehicle when the aerial vehicle is operating in the horizontal flight orientation.

    Active airborne noise abatement
    87.
    发明授权

    公开(公告)号:US10468008B2

    公开(公告)日:2019-11-05

    申请号:US15936928

    申请日:2018-03-27

    Abstract: Noises that are to be emitted by an aerial vehicle during operations may be predicted using one or more machine learning systems, algorithms or techniques. Anti-noises having equal or similar intensities and equal but out-of-phase frequencies may be identified and generated based on the predicted noises, thereby reducing or eliminating the net effect of the noises. The machine learning systems, algorithms or techniques used to predict such noises may be trained using emitted sound pressure levels observed during prior operations of aerial vehicles, as well as environmental conditions, operational characteristics of the aerial vehicles or locations of the aerial vehicles during such prior operations. Anti-noises may be identified and generated based on an overall sound profile of the aerial vehicle, or on individual sounds emitted by the aerial vehicle by discrete sources.

    Adjustable propeller blades for sound control

    公开(公告)号:US10287006B1

    公开(公告)日:2019-05-14

    申请号:US14975302

    申请日:2015-12-18

    Abstract: Sounds are generated by an aerial vehicle during operation. For example, the motors and propellers of an aerial vehicle generate sounds during operation. Disclosed are systems, methods, and apparatus for actively adjusting the shape of a propeller blade of an aerial vehicle during operation of the aerial vehicle. For example, the propeller blade may have one or more joints that adjust to alter the shape of the propeller blade. The altered shape of the propeller blade causes the propeller to generate different frequencies of sound as it rotates. By altering multiple propeller blades of the aerial vehicle, the different sounds generated by the different propeller blades may effectively cancel or reduce the total sound generated by the aerial vehicle, and/or alter the total frequency generated.

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