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Preliminary Effect of Synthetic Vision Systems Displays to Reduce Low-Visibility Loss of Control and Controlled Flight Into Terrain Accidents

机译:合成视觉系统显示器的初步效果,可减少因低能见度而造成的控制损失和受控飞行导致的地形事故

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摘要

An experimental investigation was conducted to study the effectiveness of Synthetic Vision Systems (SVS) flight displays as a means of eliminating Low Visibility Loss of Control (LVLOC) and Controlled Flight Into Terrain (CFIT) accidents by low time general aviation (GA) pilots. A series of basic maneuvers were performed by 18 subject pilots during transition from Visual Meteorological Conditions (VMC) to Instrument Meteorological Conditions (IMC), with continued flight into IMC, employing a fixed-based flight simulator. A total of three display concepts were employed for this evaluation. One display concept, referred to as the Attitude Indicator (AI) replicated instrumentation common in today's General Aviation (GA) aircraft. The second display concept, referred to as the Electronic Attitude Indicator (EAI), featured an enlarged attitude indicator that was more representative of a glass display that also included advanced flight symbology, such as a velocity vector. The third concept, referred to as the SVS display, was identical to the EAI except that computer-generated terrain imagery replaced the conventional blue-sky/brown-ground of the EAI. Pilot performance parameters, pilot control inputs and physiological data were recorded for post-test analysis. Situation awareness (SA) and qualitative pilot comments were obtained through questionnaires and free-form interviews administered immediately after the experimental session. Initial pilot performance data were obtained by instructor pilot observations. Physiological data (skin temperature, heart rate, and muscle flexure) were also recorded. Preliminary results indicate that far less errors were committed when using the EAI and SVS displays than when using conventional instruments. The specific data example examined in this report illustrates the benefit from SVS displays to avoid massive loss of SA conditions. All pilots acknowledged the enhanced situation awareness provided by the SVS display concept. Levels of pilot stress appear to be correlated with skin temperature measurements.
机译:进行了一项实验研究,以研究合成视觉系统(SVS)飞行显示器作为消除低空通用航空(GA)飞行员的低能见度失控(LVLOC)和受控飞行入地形(CFIT)事故的一种手段。在从视觉气象条件(VMC)到仪器气象条件(IMC)的过渡过程中,由18名主题飞行员进行了一系列基本操作,并继续使用固定的飞行模拟器飞往IMC。总共使用了三个显示概念进行此评估。一种显示概念,称为高度指示器(AI),是当今通用航空(GA)飞机中常用的仪表。第二种显示概念称为电子姿态指示器(EAI),其特点是具有更大的姿态指示器,该指示器更能代表玻璃显示器,其中还包括先进的飞行符号,例如速度矢量。第三个概念称为SVS显示器,与EAI相同,只是计算机生成的地形图像代替了EAI的常规蓝天/棕色地面。记录飞行员的性能参数,飞行员的控制输入和生理数据,以进行测试后分析。在实验会议结束后立即通过问卷调查和自由形式访谈获得了态势感知(SA)和定性的飞行员评论。最初的飞行员性能数据是通过教练的飞行员观察获得的。还记录了生理数据(皮肤温度,心率和肌肉弯曲)。初步结果表明,使用EAI和SVS显示器时所犯的错误要比使用常规仪器时少得多。本报告中检查的特定数据示例说明了SVS显示屏的好处,可以避免SA条件的大量损失。所有飞行员都承认SVS显示概念增强了态势感知能力。飞行员的压力水平似乎与皮肤温度测量值相关。

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