Unmanned rotorcraft and method for measuring circumjacent object around rotorcraft

    公开(公告)号:US10683086B2

    公开(公告)日:2020-06-16

    申请号:US15558058

    申请日:2016-03-22

    Inventor: Kazuo Ichihara

    Abstract: To provide an unmanned rotorcraft and a method for measuring a distance to a circumjacent objet around the rotorcraft, enabling it to prevent its airframe from colliding with a circumjacent object when flying and prevent its airframe from falling down when landing, while suppressing an increase in airframe cost. This is solved by an unmanned rotorcraft including a distance sensor to measure a distance between its airframe and a circumjacent object around it, the distance sensor and its detection direction being fixed to the airframe, and a method for measuring a distance to a circumjacent objet around the rotorcraft, adapted to watch or watch out for a circumjacent object around the airframe by turning the airframe automatically in a yaw direction under predefined conditions or to measure a difference of elevation at landing points of all legs of the airframe.

    UNMANNED AERIAL VEHICLE
    2.
    发明申请

    公开(公告)号:US20200140057A1

    公开(公告)日:2020-05-07

    申请号:US16576250

    申请日:2019-09-19

    Abstract: An unmanned aerial vehicle includes a plurality of propellers and an airframe. The airframe includes a body having a hollow portion, and a plurality of through holes connected to the hollow portion and formed on an outer peripheral surface of the body. The airframe also includes a plurality of arms supporting the plurality of propellers, and each arm of the plurality of arms includes a base end portion disposed at a body side in a longitudinal direction of the respective arm. The base end portion is inserted in a corresponding through hole of the plurality of through holes and supported by the body. Each arm of the plurality of arms is configured to be stored in the hollow portion of the body by being retracted into the body via the through hole, and expanded out of the body by being pulled out of the body via the through hole.

    METHOD FOR SETTING FLIGHT ALTITUDE OF UNMANNED AERIAL VEHICLE AND UNMANNED AERIAL VEHICLE SYSTEM

    公开(公告)号:US20200033890A1

    公开(公告)日:2020-01-30

    申请号:US16499787

    申请日:2018-07-09

    Inventor: Kiyokazu SUGAKI

    Abstract: A method for setting a flight altitude and such an unmanned aerial vehicle system that efficiently set the flight altitude in a flight plan based on undulation and/or inclination of a ground surface or a ground object. The method includes: an undulation research step of making the unmanned aerial vehicle fly and measuring a height of a ground surface or a ground object; and an altitude setting step of, during preparation of a flight plan that is setting data including a specification of a path on which the unmanned aerial vehicle is made to fly autonomously, automatically setting the flight altitude on the path in the flight plan based on the height of the ground surface or the ground object measured in the undulation research step. An unmanned aerial vehicle system capable of performing the method.

    Unmanned aerial vehicle
    4.
    发明授权

    公开(公告)号:US10427781B2

    公开(公告)日:2019-10-01

    申请号:US15566660

    申请日:2016-04-19

    Abstract: A multicopter equipped with a fall prevention device enabling it to prevent the airframe from falling even in case the multicopter has become unable to fly normally for various reasons. A multicopter includes a multicopter main body having rotors which are driven by a power source, a plurality of emergency rotors which are driven by an emergency power source which is different from the power source, abnormality detection sensors for detecting abnormality of the multicopter main body, and an emergency control device, the multicopter being configured such that, when the abnormality detection sensors have detected abnormality of the multicopter main body, the emergency control device performs control to deactivate operation of the rotors and drive the emergency rotors by the emergency power source to prevent a rapid fall of the multicopter.

    LIVING BODY SEARCH SYSTEM
    5.
    发明申请

    公开(公告)号:US20190057252A1

    公开(公告)日:2019-02-21

    申请号:US16080907

    申请日:2017-02-23

    Abstract: A living body search system includes an unmanned moving body and a server. The body includes: a camera; image data processing for retrieving image data; moving means; and communicating. The server includes: a database configured to record therein search data; and notifies a client. The body and the server are connected to each other through a communication network. The system includes individuals in the image data wherein individual identification information records the database to determine whether the candidate object in the image data is a searched-for object. The system registers, in the server, searched-for data provided in advance from the client. The system compares image data retrieved from the camera with the individual identification information to perform individual recognition. When the image data matches the individual identification information, the system determines that the object has been found. Then, the system notifies the client that the searched-for object has been found.

    ELECTRICITY GENERATING APPARATUS AND UNMANNED AERIAL VEHICLE EQUIPPED WITH SAME

    公开(公告)号:US20180134384A1

    公开(公告)日:2018-05-17

    申请号:US15567565

    申请日:2016-08-08

    Inventor: Kazuo ICHIHARA

    Abstract: An electricity generating apparatus capable of efficiently and safely charging a storage battery in an unmanned aerial vehicle during its flight and an unmanned aerial vehicle equipped with such apparatus. The apparatus is mounted in the vehicle, including a fuel tank which is a container body to reserve fuel, an electric generator unit connected to the fuel tank, tilt measurement means capable of measuring a tilt of the fuel tank, and electricity generation control means for controlling operation of generating electricity by the electric generator unit, wherein the electric generator unit is capable of charging a storage battery in the vehicle during flight, and the electricity generation control means drives the electric generator unit when a tilt angle of the fuel tank indicated by the tilt measurement means is within a safe angle which is a predetermined threshold angle, as well as an unmanned aerial vehicle equipped with such apparatus.

    ATTACHABLE-DETACHABLE UNIT AND SENSOR CALIBRATING METHOD USING THE SAME

    公开(公告)号:US20200249019A1

    公开(公告)日:2020-08-06

    申请号:US16336853

    申请日:2017-08-21

    Inventor: Kiyokazu SUGAKI

    Abstract: An attachable-detachable unit and a sensor calibrating method using the same such that the attachable-detachable unit and the sensor calibrating method make calibration work on sensors of an unmanned aerial vehicle efficient and unitize the control functions of the unmanned aerial vehicle. The problem is solved by: an attachable-detachable unit including a base made of a case or a board that is attachable and detachable to and from an airframe of an unmanned aerial vehicle, wherein a magnetic sensor constituting an electronic compass is mounted on the base; and a sensor calibrating method including a procedure for calibrating the electronic compass and/or the inertia measurement device by, with the attachable-detachable unit removed from the unmanned aerial vehicle, manually rotating the attachable-detachable unit or manually keeping the attachable-detachable unit at a predetermined posture.

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