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    Collision and conflict avoidance system for autonomous unmanned air vehicles (UAVs)
    3.
    发明授权
    Collision and conflict avoidance system for autonomous unmanned air vehicles (UAVs) 有权
    自主无人机（UAV）的碰撞冲突避免系统

    公开(公告)号：US07737878B2

    公开(公告)日：2010-06-15

    申请号：US12169205

    申请日：2008-07-08

    申请人： Joost van Tooren ,  Martin Heni ,  Alexander Knoll ,  Johannes Beck

    发明人： Joost van Tooren ,  Martin Heni ,  Alexander Knoll ,  Johannes Beck

    IPC分类号： G01S13/93 ,  G08G5/04 ,  G01S13/00 ,  G08G5/00

    CPC分类号： G08G5/0078 ,  G01S13/9303 ,  G08G5/006 ,  G08G5/0069 ,  G08G5/045

    摘要： A collision and conflict avoidance system for autonomous unmanned air vehicles (UAVs) uses accessible on-board sensors to generate an image of the surrounding airspace. The situation thus established is analyzed for imminent conflicts (collisions, TCAS violations, airspace violations), and, if a probable conflict or collision is detected, a search for avoidance options is started, wherein the avoidance routes as far as possible comply with statutory air traffic regulations. By virtue of the on-board algorithm the system functions independently of a data link. By taking into account the TCAS zones, the remaining air traffic is not disturbed unnecessarily. The system makes it possible both to cover aspects critical for safety and to use more highly developed algorithms in order to take complicated boundary conditions into account when determining the avoidance course.

    摘要翻译： 自主无人驾驶飞行器（UAV）的碰撞和冲突避免系统使用可访问的车载传感器来生成周围空域的图像。 对即将发生的冲突（冲突，TCAS违规，违反空域）进行了分析，如果发现可能的冲突或碰撞，则开始搜索避免选择，其中避免路线尽可能符合法定航空 交通条例。 凭借车载算法，系统独立于数据链路功能。 通过考虑到TCAS区域，剩余的空中交通不会被不必要的干扰。 该系统可以涵盖对安全性至关重要的方面，并且使用更高度发展的算法，以便在确定回避过程时考虑复杂的边界条件。

    Flight control display
    4.
    发明授权
    Flight control display 有权
    飞行控制显示

    公开(公告)号：US07365705B2

    公开(公告)日：2008-04-29

    申请号：US09852292

    申请日：2001-05-10

    申请人： Alexander Knoll

    发明人： Alexander Knoll

    IPC分类号： G09G5/00

    CPC分类号： G01C23/005

    摘要： An aircraft flight control display for orientation of the pilot during an approach of the aircraft toward a destination has a center of the display as its fixed point. An aircraft symbol with a center depicts the longitudinal axis as well as a lateral line to depict the current attitude of the aircraft. A destination position symbol has a reference line and a position symbol, with a skyline having a center. The destination position symbol is located at a distance from the center and its reference line points to the center as the reference point. The destination position symbol is rotated around the reference point dependent on the relative position of the aircraft's direction or the flight direction to the desired destination direction.

    摘要翻译： 在飞行器朝向目的地的接近期间飞行员的朝向的飞行器飞行控制显示器具有显示器的中心作为其固定点。 具有中心的飞机符号描绘了纵向轴线和侧线，以描绘飞机的当前姿态。 目的地位置符号具有参考线和位置符号，天际线具有中心。 目的地位置符号位于距离中心一定距离处，其参考线指向中心作为参考点。 目的地位置符号围绕参考点旋转，这取决于飞机方向或飞行方向到所需目的地方向的相对位置。

    Low-altitude flight guidance system, warning system for low-altitude flight guidance, warning generator for low-altitude flight guidance and method for low-altitude flight guidance
    5.
    发明申请
    Low-altitude flight guidance system, warning system for low-altitude flight guidance, warning generator for low-altitude flight guidance and method for low-altitude flight guidance 有权
    低空飞行导航系统，低空飞行指导预警系统，低空飞行指导警报发生器和低空飞行指导方法

    公开(公告)号：US20050049763A1

    公开(公告)日：2005-03-03

    申请号：US10927078

    申请日：2004-08-27

    申请人： Anton Walsdorf ,  Johannes Drexler ,  Lars Schopfer ,  Alexander Knoll

    发明人： Anton Walsdorf ,  Johannes Drexler ,  Lars Schopfer ,  Alexander Knoll

    IPC分类号： B64D45/04 ,  G01C5/00 ,  G05D1/06 ,  G06F17/00

    CPC分类号： G01C5/005 ,  B64D45/04 ,  G05D1/0646

    摘要： A low-altitude flight guidance system for an aircraft including a warning generator that generates a warning based upon a predicted position. The system further including a first sensor system having a terrain database and a calculation module that determines a current position of the aircraft with respect to terrain stored in the terrain database and that determines a reference altitude hDB of the terrain at the current position. The system further includes a second sensor system and a module that determines a predetermined flight altitude difference ΔhF at the predicted position and terrain data in a region U of the predicted position. Moreover, the system includes an altitude prediction module that predicts an altitude and forwards the predicted altitude to the warning generator. The warning is based upon the aircraft reaching, approaching, or exceeding a warning altitude limit, and the altitude prediction module determination for the predicted position is based upon a prediction set point. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.

    摘要翻译： 一种用于飞机的低空飞行引导系统，其包括基于预测位置产生警告的警告发生器。 该系统还包括具有地形数据库的第一传感器系统和确定飞机相对于地形数据库中存储的地形的当前位置并且确定当前位置处的地形的参考高度hDB的计算模块。 该系统进一步包括第二传感器系统和模块，其确定预测位置处的预定飞行高度差值DeltahF和预测位置的区域U中的地形数据。 此外，该系统包括高度预测模块，其预测高度并将预测高度转发到警告发生器。 该警告基于飞机到达，接近或超过警告高度极限，并且预测位置的高度预测模块确定基于预测设定点。 本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。