ANALYTIC SYSTEM AND ANALYTIC METHOD
    4.
    发明申请

    公开(公告)号:US20190104496A1

    公开(公告)日:2019-04-04

    申请号:US15574875

    申请日:2017-05-08

    申请人: Adinte, INC.

    摘要: The flight control part 201 makes the unmanned aerial vehicle fly along a flight path in a predetermined area. The radio wave acquisition part 202 acquires radio wave information including a radio wave intensity when the radio unit of the unmanned aerial vehicle detects a short-distance radio wave of the user terminal during the flight of the unmanned aerial vehicle. The flight position acquisition part 203 acquires GPS position information of the unmanned aerial vehicle when the radio unit detected the short-distance radio wave, as a flight position of the unmanned aerial vehicle based on a GPS unit of the unmanned aerial vehicle. The terminal position calculation part 204 calculates a presence position of the user terminal in the area based on a radio wave intensity of the acquired radio wave information, and the acquired flight position of the unmanned aerial vehicle. The user attribute analysis part 205 arranges the calculated presence position of the user terminal in the map information corresponding to the area, and analyzes user attribute information of the user terminal based on place attribute information indicating a characteristic of the place where the presence position is arranged.

    AN AUTONOMOUS VEHICLE CONTROL SYSTEM
    9.
    发明申请

    公开(公告)号:US20180239367A1

    公开(公告)日:2018-08-23

    申请号:US15751097

    申请日:2016-11-28

    发明人: Yair Kahn

    IPC分类号: G05D1/10 B64C39/02 G08G5/00

    摘要: A drone control system for controlling a drone which includes an onboard-flight-system previously configured to receive navigational-data in a format compliant with a standard navigational data transmission protocol. The system includes a remote-sensor and an interface. The remote sensor is located remotely from the drone and determines the position of the drone relative to the remote-sensor. The interface, coupled with the remote-sensor, produces a pseudo GPS signal indicating the position of the drone and to provide the pseudo GPS signal to an onboard-flight-system of the drone. The format of the pseudo GPS signal is fully compliant with the standard navigational data transmission protocol employed by the onboard-flight-system. The onboard-flight-system is receives inertial tracking data from an onboard inertial-measuring-unit and the pseudo GPS signal, and tracks the position of the drone by merging the inertial tracking data and the pseudo GPS signal and navigates the drone accordingly.