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首页> 外文期刊>Aviation, space, and environmental medicine. >Stability of simulated flight path control at +3 Gz in a human centrifuge.
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Stability of simulated flight path control at +3 Gz in a human centrifuge.

机译:人体离心机中+3 Gz的模拟飞行路径控制的稳定性。

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INTRODUCTION: Earlier studies have shown that naive subjects and experienced jet pilots produce exaggerated manual forces when exposed to increased acceleration (+Gz). This study was designed to evaluate whether this exaggeration affects the stability of simulated flight path control. METHODS: We evaluated naive subjects' performance in a flight simulator which either remained stationary (+1 Gz), or rotated to induce an acceleration in accordance to the simulated flight path with a mean acceleration of about +3 Gz. In either case, subjects were requested to produce a series of altitude changes in pursuit of a visual target airplane. Resulting flight paths were analyzed to determine the largest oscillation after an altitude change (Oscillation) and the mean deviation between subject and target flight path (Tracking Error). RESULTS: Flight stability after an altitude change was degraded in +3 Gz compared to +1 Gz, as evidenced by larger Oscillations (+11%) and increased Tracking Errors (+80%). These deficits correlated significantly with subjects' +3 Gz deficits in a manual-force production task. DISCUSSION: We conclude that force exaggeration in +3 Gz may impair flight stability during simulated jet maneuvers in naive subjects, most likely as a consequence of vestibular stimulation.
机译:简介:较早的研究表明,天真受试者和经验丰富的喷射飞行员在加速度增加(+ Gz)时会产生过大的手动力。本研究旨在评估这种夸张是否影响模拟飞行路径控制的稳定性。方法:我们在飞行模拟器中评估了天真的受试者的表现,该模拟器要么保持静止(+1 Gz),要么根据模拟的飞行路径旋转以感应加速度,平均加速度约为+3 Gz。无论哪种情况,都要求受试者产生一系列高度变化,以追求视觉目标飞机。分析所得的飞行路径,以确定高度变化(振荡)后的最大振荡以及对象与目标飞行路径之间的平均偏差(跟踪误差)。结果:相比于+1 Gz,海拔变化后的飞行稳定性在+3 Gz中下降,这由较大的振荡(+ 11%)和增加的跟踪误差(+ 80%)证明。这些缺陷与手动生产任务中受试者的+3 Gz缺陷显着相关。讨论:我们得出结论,在天真受试者的模拟射流操纵中,+ 3 Gz的力夸大可能会损害飞行稳定性,这很可能是前庭刺激的结果。

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