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Sensor based 3D conformal cueing for safe and reliable HC operation specifically for landing in DVE

机译:基于传感器的3D保形提示可实现安全可靠的HC操作,专门用于DVE中的着陆

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The paper describes the approach of a sensor based landing aid for helicopters in degraded visual conditions. The system concept presented employs a long range high resolution ladar sensor allowing for identifying obstacles in the flight and in the approach path as well as measuring landing site conditions like slope, roughness and precise position relative to the helicopter during long final approach. All these measurements are visualized to the pilot. Cueing is done by 3D conformal symbology displayed in a head-tracked HMD enhanced by 2D symbols for data which is perceived easier by 2D symbols than by 3D cueing. All 3D conformal symbology is placed on the measured landing site surface which is further visualized by a grid structure for displaying landing site slope, roughness and small obstacles. Due to the limited resolution of the employed HMD a specific scheme of blending in the information during the approach is employed. The interplay between in flight and in approach obstacle warning and CFIT warning symbology with this landing aid symbology is also investigated and exemplarily evaluated for the NH90 helicopter which has already today implemented a long range high resolution ladar sensor based obstacle warning and CFIT symbology. The paper further describes the results of simulator and flight tests performed with this system employing a ladar sensor and a head-tracked head mounted display system. In the simulator trials a full model of the ladar sensor producing 3D measurement points was used working with the same algorithms used in flight tests.
机译:本文介绍了在视觉条件下降的情况下,基于传感器的直升机着陆辅助装置的方法。提出的系统概念采用远程高分辨率雷达传感器,该传感器可识别飞行中和进近路径中的障碍物,并在长时间最终进近过程中测量着陆点条件,例如倾斜度,粗糙度和相对于直升机的精确位置。所有这些测量结果都将可视化显示给飞行员。提示是通过在头部跟踪的HMD中显示的3D保形符号来完成的,该头戴式显示器的2D符号增强了数据,而2D符号比3D提示更易于感知。所有3D保形符号系统都放置在测量的着陆点表面上,并通过网格结构进一步可视化,以显示着陆点的坡度,粗糙度和小的障碍物。由于所采用的HMD的分辨率有限,因此采用了在该方法期间将信息混合的特定方案。还针对NH90直升机对飞行中和进近障碍物警告与CFIT警告符号体系与这种着陆辅助符号体系之间的相互作用进行了调查并进行了示例性评估,NH90直升机现已实施了基于远程高分辨率雷达传感器的障碍物警告和CFIT符号体系。本文进一步描述了使用该系统使用雷达传感器和头戴式头戴式显示系统进行的模拟器和飞行测试的结果。在模拟器试验中,使用了产生3D测量点的激光传感器的完整模型,并使用了与飞行测试中使用的算法相同的算法。

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