Target tracking method for air vehicle
    42.
    发明申请

    公开(公告)号:US20180107229A1

    公开(公告)日:2018-04-19

    申请号:US15582662

    申请日:2017-04-29

    CPC classification number: G05D1/12 G05D1/0094 G05D1/102

    Abstract: A target tracking method for an air vehicle includes steps of: during a flight of an air vehicle main body to a position corresponding to a global positioning system (GPS) positioning signal, taking pictures of an area where a reference target is located by a camera, and obtaining a reference image; extracting reference image characteristics of the reference target and initial position information of the reference target in the reference image from the reference image; when the camera obtains a temporary image showing a temporary target, extracting temporary image characteristics of the temporary target and temporary position information of the temporary target in the temporary image from the temporary image; if the reference image characteristics are consistent with the temporary image characteristics, calculating a deviation direction according to a difference between the initial position information and the temporary position information; and tracking the temporary target in the deviation direction.

    Control System, Terminal and Airborne Flight Control System of Multi-rotor Craft

    公开(公告)号:US20180046203A1

    公开(公告)日:2018-02-15

    申请号:US15555520

    申请日:2015-04-09

    Inventor: Huazhi Hu

    Abstract: A control system includes an airborne flight control system and a smart terminal; the airborne flight control system is configured to acquire a first position information, and send the first position information to the smart terminal; the smart terminal is configured to acquire a second position information, and obtain a yaw angle and at least one of a horizontal flight speed and a vertical flight speed according to the second position information and the first position information sent by the airborne flight control system, and send the yaw angle and at least one of the horizontal flight speed and the vertical flight speed to the airborne flight control system, wherein the first position information is the position information of an aircraft where the airborne flight control system is located, and the second position information is the position information of the smart terminal.

    Dynamic Collision-Avoidance System and Method

    公开(公告)号:US20170301249A1

    公开(公告)日:2017-10-19

    申请号:US15291892

    申请日:2016-10-12

    CPC classification number: G08G5/045 G05D1/0088 G05D1/101 G05D1/102

    Abstract: An obstacle-avoidance system for a vehicle, the obstacle-avoidance system may comprise: a communication device; a plurality of sensors, the plurality of sensors configured to detect collision threats within a predetermined distance of the vehicle; and a processor. The processor may communicatively couple to the communication device and the plurality of sensors and configured to receive navigation commands being communicated to a control system via said communication device. The processor may also receive, from at least one of said plurality of sensors, obstruction data reflecting the position of an obstruction. Using the obstruction data, the processor identifies a direction for avoiding said obstruction. In response, the processor may output, via said communication device, a derivative command to said control system causing the vehicle to travel in said flight direction.

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