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A pilot evaluation of movable and rigid aircraft controls.

机译:对可移动和刚性飞机控制装置的飞行员评估。

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摘要

A simulator facility employing a two-axis compensatory trackingtask with a random-appearing signal was used to evaluate the performanceof fifty-five pilot and non-pilot test subjects using four separatecontrol sticks — two movable and two rigid. Pilot acceptance of therigid cockpit controllers was determined by comparing individual pilotratings of the sticks. In general, in both performance and opinion, therigid systems were found to be superior to their movable counterparts.Steps were taken to avoid errors due to pilot bias, learning, adaptation,or fatigue. The results obtained are subject to several test limitations,including the low stick-force levels used, the neglect of aircraftvibration effects, and the realism of the simulation.
机译:使用带有随机出现信号的两轴补偿跟踪任务的模拟器设施,使用四个单独的控制杆(两个可动杆和两个刚性杆)评估了55名飞行员和非飞行员测试对象的性能。刚性驾驶舱控制器的驾驶员接受度是通过比较各个操纵杆的操纵度来确定的。总的来说,从性能和观点来看,刚性系统都优于可动系统,并采取措施避免因飞行员偏见,学习,适应或疲劳引起的误差。获得的结果受到几个测试限制,包括使用的低粘力水平,对飞机振动效应的忽视以及模拟的真实性。

著录项

  • 作者

    Cole James Daniel;

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  • 年度 1970
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