Influence of Optical and Gravito-Inertial Cues to Height Perception During Supervisory Control

Martine Godfroy-Cooper, E. Bachelder, J. Miller, Sjsu, Add, AvMC, Francois Denquin, J. Sarrazin, Icna, Dtis, Onera
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引用次数: 1

Abstract

Future vertical lift (FVL) missions will be characterized by increased agility, degraded visual environments (DVE) and optionally piloted vehicles (OPVs). Increased agility will induce more frequent variations of linear and angular accelerations, while DVE will reduce the structure and quality of the out-the-window (OTW) scene (i.e. optical flow). As helicopters become faster and more agile, pilots are expected to navigate at low altitudes while traveling at high speeds. In nap of the earth (NOE) flights, the perception of self-position and orientation provided by visual, vestibular, and proprioceptive cues can vary from moment to moment due to visibility conditions and body alignment as a response to gravitoinertial forces and internally/externally induced perturbations. As a result, erroneous perceptions of the self and the environment can arise, leading ultimately to spatial disorientation (SD). In OPV conditions, the use of different autopilot modes implies a modification of pilot role from active pilot to systems supervisor. This shift in paradigm, where pilotage is not the primary task, and where feedback from the controls is no more available, is not without consequences. Of importance is the evidence that space perception and its geometric properties can be strongly modulated by the active or passive nature of the displacement in space. An experiment was conducted using the vertical motion simulator (VMS) at the NASA Ames Research Center that examined the contributions of gravitoinertial cueing and visual cueing in a task where the pilot was not in control of the aircraft but was asked to perform altitude monitoring in a simulated UH-60 Black Hawk helicopter with a simulated autopilot (AP) mode. Within the altitude monitoring task, the global optical density (OD), flow rate and visual level of detail (LOD) were manipulated by the introduction of an 18ft vertical drift, upward or downward that simulates a vertical wind shift. Seven pilots were tested in two visual meteorological conditions, good visual environment (GVE) and degraded visual environment (DVE) and two gravitoinertial conditions, where platform motion was either ON or OFF. The results showed that both the good quality of the visual environment and the presence of gravitoinertial cues improved altitude awareness and reduced detection/ reaction times. The improvement of the tracking performance in the visuo-vestibular setting as compared to a visual only setting when the visual cues were poor indicated some level of multisensory integration. Task-dependent limitations of a popular aeronautics metric called DIMSS-PM (Dynamic Interface Modeling and Simulation System Product Metric) and its sub-components were shown, and recommendations for OPV operations were formulated.
光学和重力惯性线索对监督控制过程中高度感知的影响
未来垂直升力(FVL)任务的特点将是灵活性提高、视觉环境退化(DVE)和可选驾驶车辆(opv)。敏捷性的提高将导致线性和角加速度的更频繁变化,而DVE将降低窗外(OTW)场景(即光流)的结构和质量。随着直升机变得更快、更灵活,飞行员有望在高速飞行的同时在低空飞行。在地球上的小睡(NOE)飞行中,由于可见性条件和身体对重力惯性力和内部/外部诱导扰动的响应,视觉、前庭和本体感觉线索提供的自我位置和方向感知可能随时变化。因此,会产生对自我和环境的错误认知,最终导致空间定向障碍(SD)。在OPV条件下,使用不同的自动驾驶模式意味着驾驶员角色从主动驾驶员转变为系统监督者。这种模式的转变,即引航不是主要任务,来自控制的反馈不再可用,并不是没有后果的。重要的是,有证据表明,空间感知及其几何特性可以受到空间中位移的主动或被动性质的强烈调节。利用美国宇航局艾姆斯研究中心的垂直运动模拟器(VMS)进行了一项实验,该实验检查了重力惯性提示和视觉提示在飞行员不控制飞机但被要求在模拟的UH-60黑鹰直升机上进行高度监测的任务中的贡献,该直升机具有模拟自动驾驶仪(AP)模式。在高度监测任务中,全球光密度(OD)、流速和视觉细节水平(LOD)通过引入18英尺的垂直漂移(向上或向下)来模拟垂直风移来控制。7名飞行员在两种视觉气象条件、良好视觉环境(GVE)和退化视觉环境(DVE)以及两种重力惯性条件下进行了测试,其中平台运动处于ON或OFF状态。结果表明,良好的视觉环境质量和重力惯性提示的存在提高了高度感知能力,缩短了探测/反应时间。当视觉线索较差时,在视觉-前庭环境中跟踪表现的改善表明了某种程度的多感觉整合。展示了一种名为DIMSS-PM(动态接口建模与仿真系统产品度量)的流行航空度量及其子组件的任务依赖限制,并制定了OPV操作的建议。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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