Wickens Christopher D, Self Brian P, Small Ronald L, Williams Choi B, Burrows Christina L, Levinthal Brian R, Keller John W
Alion Science and Technology Corp., Boulder, CO 80301, USA.
Aviat Space Environ Med. 2006 Dec;77(12):1244-51.
Aviation spatial disorientation mishaps remain a concern, especially due to their fatality rate. Some of the most insidious disorientations are due to vestibular stimuli in the absence of visual cues. A category of such disorientations are known as somatogyral illusions.
To determine the effects of spin rate and duration on the perception of the somatogyral illusion, we examined the subjective response of pilots and non-pilots to rotation around the yaw axis in a flight simulator in a manner that would mimic two vestibular illusions found in flight: the washout of the semi-circular canals following sustained turns, and the illusory counter-rotation following return to straight and level flight. There were 29 subjects (14 pilots) who were seated blindfolded in a flight simulator which accelerated to constant plateau rotation rates of 20, 70, and 120 degrees x s(-1) and then decelerated to stationary; plateaus were 10, 20, or 40 s. Subjects reported 1) the time when the perception of rotation ceased (i.e., the subjective time until washout was reached); 2) the relative magnitude of the counter-rotation experienced; and 3) the time until the perception of counter-rotation ceased. Subjects also manipulated a slider to provide a continuous subjective measure of their experience of rotation.
The two time measures increased with increases in both the duration and magnitude of the spin. The increase in perceived washout time with spin rate was non-linear (geometric). There was an interaction between spin duration and spin rate on the experience of illusory counter-rotation magnitude such that at low rates, spin duration had no effect, but its effect increased at faster rates. The time constant of adaptation of the semicircular canals was estimated to be 8.3 s.
The effects were validated against a model of semicircular canal and cupola adaptation, which predicted the data with high accuracy. Pilots and non-pilots did not differ in their illusory experience.
航空空间定向失误仍然令人担忧,尤其是考虑到其死亡率。一些最隐匿的定向失误是由于在没有视觉线索的情况下出现前庭刺激。这类定向失误中的一种被称为躯体旋动幻觉。
为了确定旋转速率和持续时间对躯体旋动幻觉感知的影响,我们以模拟飞行中发现的两种前庭幻觉的方式,研究了飞行员和非飞行员在飞行模拟器中绕偏航轴旋转时的主观反应:持续转弯后半规管的消退,以及恢复直线平飞后的虚幻反向旋转。29名受试者(14名飞行员)被蒙住眼睛坐在飞行模拟器中,模拟器加速至20、70和120度×秒⁻¹的恒定平台旋转速率,然后减速至静止;平台持续时间为10、20或40秒。受试者报告了:1)旋转感知停止的时间(即达到消退的主观时间);2)所经历的反向旋转的相对大小;3)反向旋转感知停止的时间。受试者还操作一个滑块以提供其旋转体验的连续主观测量值。
这两个时间测量值随旋转持续时间和大小的增加而增加。感知到的消退时间随旋转速率的增加呈非线性(几何)变化。在虚幻反向旋转大小的体验方面,旋转持续时间和旋转速率之间存在交互作用,使得在低速率时,旋转持续时间没有影响,但在较快速率时其影响增加。半规管的适应时间常数估计为8.3秒。
这些效应通过半规管和顶帽适应模型得到验证,该模型对数据的预测具有很高的准确性。飞行员和非飞行员在幻觉体验方面没有差异。