首页> 外文会议>Human Factors and Ergonomics Society annual meeting;HFES 2008 >A Flight Test Evaluation of the Arc Segment Attitude Reference for Use as a Primary Flight Reference in Helmet-Mounted Displays
【24h】

A Flight Test Evaluation of the Arc Segment Attitude Reference for Use as a Primary Flight Reference in Helmet-Mounted Displays

机译:弧段姿态参考的飞行测试评估,用作头盔式显示器中的主要飞行参考

获取原文

摘要

The objective of this evaluation was to determine if the use of the Arc Segment Attitude Reference (ASAR) symbology in a head-up display (HUD) in place of the legacy climb-dive ladder attitude reference aids in unusual attitude recovery (UAR) piloting tasks as specified in AFM 11 -217 for use as a primary flight reference (PFR). Flight tests were conducted at the US Air Force Test Pilot School (TPS), Edwards AFB, California on the NF-16D Variable-stability In-flight Simulator Test Aircraft (VISTA). Five VISTA flight UAR test sorties were flown. The time for the pilot to initiate a recovery was measured in addition to the correctness of the recovery. The flight tests were conducted with the use of the HUD combiner on VISTA to examine three symbology configurations. Each of the symbology configurations, the Mil-Std-1787C HUD, dual-articulated (DA) HUD, and ASAR HUD were evaluated by five pilots for the UAR task. The flight test results revealed the ASAR resulted in faster stick input for correction of UARs then the Mil-Std-1787C HUD. This study along with other supporting research indicates that the configural design properties of the ASAR support the ability of pilots to quickly ascertain aircraft attitude.
机译:评估的目的是确定在平视显示器(HUD)中使用弧段姿态参考(ASAR)符号系统代替传统的爬升潜水俯冲式姿态参考是否有助于异常姿态恢复(UAR)驾驶AFM 11 -217中指定的任务,用作主要飞行参考(PFR)。飞行测试是在加利福尼亚州爱德华兹空军基地的美国空军测试飞行员学校(TPS)上进行的NF-16D可变稳定性飞行模拟器测试飞机(VISTA)上进行的。进行了五次VISTA飞行UAR测试飞行。除了恢复的正确性之外,还测量了飞行员启动恢复的时间。使用VISTA上的HUD组合器进行了飞行测试,以检查三种符号配置。每个符号系统配置,Mil-Std-1787C HUD,双铰接(DA)HUD和ASAR HUD由UAR任务的五个飞行员进行了评估。飞行测试结果显示,与Mil-Std-1787C HUD相比,ASAR可以更快地输入操纵杆以校正UAR。这项研究以及其他支持研究表明,ASAR的配置设计特性支持飞行员快速确定飞机姿态的能力。

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