HARVESTER WITH A SENSOR MOUNTED ON AN AIRCRAFT
    201.
    发明申请
    HARVESTER WITH A SENSOR MOUNTED ON AN AIRCRAFT 有权
    带传感器的收割机安装在飞机上

    公开(公告)号:US20120029732A1

    公开(公告)日:2012-02-02

    申请号:US13187696

    申请日:2011-07-21

    Abstract: A sensor for monitoring a plant population in front of a harvester and a transfer process of the crop from the harvester to a transport vehicle is arranged on an unmanned aircraft. The aircraft moves in the vicinity of the harvester in the harvesting mode and communicates in a wireless fashion with a control unit that controls an actuator for influencing an operating parameter of the harvester and/or the transport vehicle (in real time based on signals of the sensor in the harvesting mode.

    Abstract translation: 用于监测收割机前面的植物种群的传感器和从收割机到运输车辆的作物的转移过程被安排在无人驾驶飞机上。 飞机以收割模式在收割机附近移动,并以无线方式与控制单元进行通信,该控制单元控制用于影响收割机和/或运输车辆的操作参数的致动器(基于 传感器处于收获模式。

    Controlling movement of an unmanned vehicle
    204.
    发明授权
    Controlling movement of an unmanned vehicle 有权
    控制无人驾驶车辆的运动

    公开(公告)号:US07873444B1

    公开(公告)日:2011-01-18

    申请号:US11704030

    申请日:2007-02-08

    Abstract: An unmanned vehicle (UV) embodiment can include a motor for movement of the UV in at least two dimensions, a receiver mechanism for receiving communication from the control station, a control unit for controlling the actuation of the motor, and memory having instructions stored thereon and executable by the control unit to, utilize environmental information to maintain the UV in a stable position and to move the UV according to control information received from the control station.

    Abstract translation: 无人驾驶车辆(UV)实施例可以包括用于在至少两个维度上移动UV的电动机,用于从控制站接收通信的接收机构,用于控制电动机的致动的控制单元和具有存储在其上的指令的存储器 并且可由控制单元执行,利用环境信息将UV维持在稳定位置,并根据从控制站接收的控制信息移动UV。

    Aircraft control system
    205.
    发明申请
    Aircraft control system 有权
    飞机控制系统

    公开(公告)号:US20030141409A1

    公开(公告)日:2003-07-31

    申请号:US10310415

    申请日:2002-12-05

    Abstract: A solar rechargeable, long-duration, span-loaded flying wing, having no fuselage or rudder. Having a two-hundred foot wingspan that mounts photovoltaic cells on most all of the wing's top surface, the aircraft uses only differential thrust of its eight propellers to turn, pitch and yaw. The wing is configured to deform under flight loads to position the propellers such that the control can be achieved. Each of five segments of the wing has one or more motors and photovoltaic arrays, and produces its own lift independent of the other segments, to avoid loading them. Five two-sided photovoltaic arrays, in all, are mounted on the wing, and receive photovoltaic energy both incident on top of the wing, and which is incident also from below, through a bottom, transparent surface.

    Abstract translation: 太阳能可再充电,长时间,跨度的飞翼,没有机身或方向舵。 拥有两百英尺的翼展,将光伏电池安装在大部分机翼的顶部表面上,飞机只使用其八个螺旋桨的差速推力来转弯,俯仰和偏航。 机翼构造成在飞行载荷下变形以定位螺旋桨,使得可以实现控制。 翼的五个部分中的每一个具有一个或多个电动机和光伏阵列,并且独立于其它部分产生其自身的升降机,以避免加载它们。 五个双面光伏阵列总体上安装在机翼上,并且接收能量入射到机翼的顶部并且从下方入射的光能通过底部的透明表面。

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