Method, system and apparatus for aligning a removable sensor on a vehicle

    公开(公告)号:US11639234B2

    公开(公告)日:2023-05-02

    申请号:US16393376

    申请日:2019-04-24

    Abstract: A method for aligning a removable sensor on a vehicle includes connecting the removable sensor to a sensor mounting device. The method further includes connecting a connector of an alignment apparatus to either (i) the removable sensor such that a spatial reference component of the alignment apparatus has a known position and orientation relative to a current position and orientation of the removable sensor or (ii) a fixed connection location on the vehicle such that the spatial reference component indicates a desired position and orientation of the removable sensor. In addition the method includes adjusting the current position and orientation of the removable sensor by reference to the alignment apparatus to cause the current position and orientation of the removable sensor to match the desired position and orientation of the removable sensor.

    Systems and Methods for Overriding Autonomous Control of a Device

    公开(公告)号:US20220194561A1

    公开(公告)日:2022-06-23

    申请号:US17533237

    申请日:2021-11-23

    Abstract: Within examples, a system is described that includes a control lever for controlling operation of a device, a first actuator coupled to the control lever via a rod, and a resettable frangible link coupling a second actuator to the control lever via the rod. The resettable frangible link enables separation of coupling of the second actuator from the control lever based on an applied force to the rod by the first actuator.

    Flight control cable sensor for an aircraft

    公开(公告)号:US11203415B2

    公开(公告)日:2021-12-21

    申请号:US16212648

    申请日:2018-12-06

    Abstract: Disclosed herein is a flight control cable sensor for detecting actuation of a flight control cable of an aircraft. The flight control cable sensor comprises a draw wire encoder, comprising an extendable-retractable wire. The flight control cable sensor further comprises a first connector, co-movably fixed to the extendable-retractable wire, and a second connector, co-movably fixable to the flight control cable and configured to removably co-movably engage the first connector up to a predetermined pull-off force.

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