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The Pilot's Compensatory Controllability Effected by the Angular Motion Cue

机译:角运动提示影响飞行员的补偿性

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This paper presents the result of a study thatreached the effect of pitch angular motion cue for the pilot compensatory controllability with moving based flight simulator. In order to understand the influence of angular motion cue for the human pilot in a flying airplane, this study carries out the fundamental experiments in which the pilot compensates to keep level flight for the pitch angular error from turbulence. To analyze the effect of motion cue from many directions, the motion cue was produced by varied of realization level using moving based flight simulator. The model of airplane in simulator is P2V—7's model that was limited longitudinal input and moving. The turbulence model is Dryden's turbulence model in which also limited longitudinal. This experimental results show that the control behavior and workload of the pilot are changed a little by the angular motion cue.
机译:本文提出了一项研究结果,该研究达到了俯仰角运动提示对基于移动的飞行模拟器的飞行员补偿可控性的影响。为了了解角运动提示对飞行中的飞行员的影响,本研究进行了一些基本实验,在这些实验中,飞行员对湍流产生的俯仰角误差进行了补偿,以保持水平飞行。为了从多个方向分析运动提示的效果,使用基于移动的飞行模拟器通过实现水平的变化来产生运动提示。模拟器中的飞机模型是P2V-7模型,该模型限制了纵向输入和移动。湍流模型是Dryden的湍流模型,其中纵向也受到限制。该实验结果表明,驾驶员的控制行为和工作量因角运动提示而略有变化。

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