首页> 外文会议>Conference on degraded visual environments: enhanced, synthetic, and external vision solutions >Sensor based 3D conformal cueing for safe and reliable HC operation specifically for landing in DVE
【24h】

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共形状,用于安全可靠的HC操作,专门用于降落在DVE中

获取原文

摘要

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:本文介绍的基于传感器着陆辅助用于在退化视觉条件直升飞机的方法。提出的系统的概念采用长范围内具有高分辨率激光雷达传感器,允许用于识别障碍在飞行,并在接近路径以及长最终进场期间测量着陆点条件像斜率,粗糙度和相对精确的位置到直升机。所有这些测量可视化的领航者。提示是由三维适形符号在由用于由2D符号不是由3D提示感知更简便的数据2D符号增强头部跟踪HMD显示完成。所有三维适形符号被放置在测量的着陆点表面是由网格结构进一步可视化显示着陆点斜率,粗糙度和小障碍物上。由于所采用的HMD的分辨率有限,采用在该方法过程中的信息混合的具体方案。在飞行中和的办法障碍警告和警告CFIT符号与此着陆辅助符号之间的相互作用进行了研究和示范性地评价了NH90直升机它已经实施的今天远距离高分辨率激光雷达传感器基于障碍物预警和CFIT符号。本文进一步描述了与采用激光雷达传感器和头部跟踪头戴式显示器系统该系统进行仿真和飞行试验的结果。在模拟器试验产生三维测量点的激光雷达传感器的一个完整的模型是在飞行试验中使用的相同的算法使用的工作。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号