Hysteresis-controlled DC-DC boost converter for aerial vehicles

    公开(公告)号:US10536078B2

    公开(公告)日:2020-01-14

    申请号:US15717087

    申请日:2017-09-27

    Abstract: A power conversion unit may include two or more power modules for providing high-voltage direct current power to electrical loads, such as one or more propulsion motors aboard an aerial vehicle. Each of the power modules may be controlled by hysteresis, and may include one or more pairs of transistors that are switched by a gate driver with respect to differences between a reference current and a sensed current passing through a boost inductor. The number, size and shape of the power modules may be selected to accommodate the electrical loads, and may be switched on or off, as necessary. The power conversion unit may feature at least one more power module than is required to meet all anticipated electrical loads, thereby ensuring that the power conversion unit may continue to provide power even in the event that one of the power modules experiences a fault of any kind.

    UNMANNED AERIAL VEHICLE CONFIGURATION FOR EXTENDED FLIGHT
    5.
    发明申请
    UNMANNED AERIAL VEHICLE CONFIGURATION FOR EXTENDED FLIGHT 有权
    用于扩展飞行的无人驾驶航空器配置

    公开(公告)号:US20160129998A1

    公开(公告)日:2016-05-12

    申请号:US14538570

    申请日:2014-11-11

    Abstract: This disclosure describes a configuration of an unmanned aerial vehicle (UAV) that will facilitate extended flight duration. The UAV may have any number of lifting motors. For example, the UAV may include four lifting motors (also known as a quad-copter), eight lifting motors (octo-copter), etc. Likewise, to improve the efficiency of horizontal flight, the UAV also includes a pushing motor and propeller assembly that is oriented at approximately ninety degrees to one or more of the lifting motors. When the UAV is moving horizontally, the pushing motor may be engaged and the pushing propeller will aid in the horizontal propulsion of the UAV.

    Abstract translation: 本公开描述了将有助于延长飞行持续时间的无人驾驶飞行器(UAV)的配置。 无人机可能有任何数量的起重马达。 例如,无人机可以包括四台起重电动机(也称为四号机),八台起重马达(八重直升机)等。同样,为了提高水平飞行的效率,无人机还包括一个推动马达和螺旋桨 组件,其定向在一个或多个起重马达上大约九十度。 当无人机水平移动时,推动马达可以接合,推进螺旋桨将有助于无人机的水平推进。

    Automated pre-flight and in-flight testing of aerial vehicles by machine learning

    公开(公告)号:US10810501B1

    公开(公告)日:2020-10-20

    申请号:US15789185

    申请日:2017-10-20

    Abstract: Data captured during evolutions performed by aerial vehicles prior to one or more missions, and data regarding outcomes of the missions, may be used to train a machine learning system to predict data regarding an outcome of a mission of an aerial vehicle based on the performance of the aerial vehicle during one or more evolutions. The data may be captured by sensors provided aboard an aerial vehicle, or in association with a testing facility, and may include data captured during both pre-flight and/or in-flight evolutions performed by the aerial vehicle. The evolutions may include any pre-flight operation of motors, propellers and/or control surfaces, or any other components, as well as the in-flight operation of such components. If a machine learning system determines that a mission is unlikely to succeed, the mission may be canceled, delayed until further inspections may be performed, or assigned to another aerial vehicle.

    Hysteresis-controlled DC-DC boost converter for aerial vehicles

    公开(公告)号:US11469673B2

    公开(公告)日:2022-10-11

    申请号:US16740305

    申请日:2020-01-10

    Abstract: A power conversion unit may include two or more power modules for providing high-voltage direct current power to electrical loads, such as one or more propulsion motors aboard an aerial vehicle. Each of the power modules may be controlled by hysteresis, and may include one or more pairs of transistors that are switched by a gate driver with respect to differences between a reference current and a sensed current passing through a boost inductor. The number, size and shape of the power modules may be selected to accommodate the electrical loads, and may be switched on or off, as necessary. The power conversion unit may feature at least one more power module than is required to meet all anticipated electrical loads, thereby ensuring that the power conversion unit may continue to provide power even in the event that one of the power modules experiences a fault of any kind.

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