Abstract:
특정항공기가가시선침투요건을준수하면서특정시점에서상기지형에서주어지는위치위에서조종할수 있는지여부를계산하기위한방법및 시스템이제공된다. 상기시스템은항공기의근처에위치되는지형의적어도한 영역을나타내는 3D 모델을저장하도록구성되는컴퓨터메모리, 상기지형의상기영역을적어도두가지유형으로매핑하도록구성되는컴퓨터프로세서를포함하며, 제1 유형은가시선침투를준수하면서각각의지형위에서조종하도록상기항공기의포텐셜을나타내고, 제2 유형은상기가시선침투를준수하면서각각의지형을위에서조종하도록상기항공기의비포텐셜을지시하며, 상기매핑은상기파라미터들, 상기 3D 모델및 항공기의주어지는성능에기초하여수행된다.
Abstract:
PROBLEM TO BE SOLVED: To provide a vehicle mounted image processing system and method enabling selective imaging of objects in a low-visibility environment. SOLUTION: A vehicle mounted night vision image processing system includes a light source providing invisible light pulses and a camera having an image intensifier enabled to gate selected received images. The light source may be a laser generator, which may be enabled to generate a pulse width related to the width of a field to be imaged. The gated image intensifier may determine gating time spans according to the width of a field to be imaged. COPYRIGHT: (C)2010,JPO&INPIT
Abstract in simplified Chinese:第一热管理方法包括具有多个气流信道的空气流动通过冷却机构,用于散去PCA中产生的热。通过至少一信道的空气流动方向系不同于通过至少另一信道的空气流动方向。替代地或额外地,至少一信道的气流入口相对于气流出口为离轴的。第二热管理方法包括借由减轻通孔裂化或PTH疲劳来制造具有增强的耐久性的PCB。至少一PCB层包括:形成自3D织造玻璃钢织物之基底材料;以及沉积在基底材料表面上的导电材料。导电PTH延伸通过多个PCB层的基底材料,其中基底材料沿着Z轴方向的CTE实质上匹配于导电材料沿着x轴方向的CTE。
Abstract in simplified Chinese:本发明是陆用车辆武器系统包含一与陆用车辆结合的基座架,一武器架,复数个与武器架结合的武器,一结合在基座架与武器架之间的武器移动机构,复数个与基座架、武器架、武器及武器移动机构其中至少一个结合的移动组件,一与武器架、武器及基座架其中至少一个结合的传感机构,及至少一个与武器、武器移动机构、移动组件及传感机构结合的用户界面,且用户界面能让用户远距操控武器,武器移动机构可操作为在多个组态间移动武器。
Abstract:
A weight estimation system for estimating weight of an aerospace vehicle while grounded, the weight estimation system comprising a measurement subsystem including at least one sensor configured to measure a physical property in an interface that interfaces at least one of a fuselage and a wing with an undercarriage of said aerospace vehicle, in at least one area exhibiting a measurable change in geometry that is at least partly due to said weight, said measurement subsystem configured to produce measured data indicative of said weight of said aerospace vehicle; and a processor for receiving at least part of said measured data, said processor configured to estimate said weight, by relating said measured data with predetermined physical-property-to-weight correspondence data associated with said aerospace vehicle.