AERIAL VEHICLE
    1.
    发明申请

    公开(公告)号:US20220363374A1

    公开(公告)日:2022-11-17

    申请号:US17767054

    申请日:2019-10-08

    摘要: To provide an aerial vehicle that can improve the driving feel and riding comfort of a rider. An aerial vehicle according to the present technology includes: a vehicle body extending in the front-rear direction; a saddle section provided on an upper side of the vehicle body; a motive power section provided on an underside of the vehicle body, at a position below the saddle section; and a rotary wing section which is provided at at least one of the front and rear of the motive power section, and which rotates by using the motive power section as a motive power source.

    AERIAL VEHICLE
    2.
    发明申请

    公开(公告)号:US20220380032A1

    公开(公告)日:2022-12-01

    申请号:US17767055

    申请日:2019-10-08

    IPC分类号: B64C27/20 B64C13/04 B64C27/08

    摘要: To provide an aerial vehicle that can realize ease of operation during driving. An aerial vehicle according to the present technology includes: a vehicle body extending in a front-rear direction; a saddle section provided on an upper side of the vehicle body; a grip section provided on the front side of the saddle section in the vehicle body; and a rotary wing section which is provided in the vehicle body and which generates lift and/or thrust with respect to the vehicle body; wherein an operation section for performing operations pertaining to actions relating to ascent and/or propulsion of the vehicle body is provided in the grip section.

    FLYING OBJECT AND SYSTEM
    3.
    发明申请

    公开(公告)号:US20230030547A1

    公开(公告)日:2023-02-02

    申请号:US17788283

    申请日:2020-01-07

    IPC分类号: B64C29/02 B64C39/02

    摘要: A flying object according to the present technology includes: an airframe including a rotary wing part; a plurality of sensors each provided on a bottom side of the airframe, detecting an opposed surface, and measuring a distance from the surface; and a control device including an estimation unit that estimates an attitude of the airframe with respect to the surface on a basis of the distance at each position of the sensors obtained from the plurality of sensors.