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Functional testing of space flight induced changes in tonic motor control by using limb-attached excitation and load devices

机译:使用肢体连接的激励和负载装置对太空飞行引起的强直性电动机控制变化进行功能测试

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摘要

Long term space flights induce atrophy and contractile changes on postural muscles such effecting tonic motor control. Functional testing of tonic motor control structures is a challenge because of the difficulties to deliver appropriate test forces on crew members. In this paper we propose two approaches for functional testing by using limb attached loading devices. The first approach is based on a frequency and amplitude controllable moving magnet exciter to deliver sinusoidal test forces during limb postures. The responding limb deflection is recorded by an embedded accelerometer to obtain limb impedance. The second approach is based on elastic limb loading to evoke self-excited oscillations during arm extensions. Here the contraction force at the oscillation onset provides information about limb stiffness. The rationale for both testing approaches is based on Feldman's λ-model. An arm expander based on the second approach was probed in a 6-month MIR space flight. The results obtained from the load oscillations, confirmed that this device is well suited to capture space flight induced neuromuscular changes.
机译:长期的太空飞行会导致姿势肌肉萎缩和收缩变化,从而影响强直运动控制。由于难以向机组人员提供适当的测试力,因此对强力电动机控制结构进行功能测试是一项挑战。在本文中,我们提出了两种使用肢体连接加载设备进行功能测试的方法。第一种方法是基于频率和幅度可控制的移动磁体激励器,以在肢体姿势期间传递正弦测试力。嵌入式加速度计记录肢体的响应,以获得肢体阻抗。第二种方法是基于弹性肢体负载,以在手臂伸展过程中引起自激振荡。在此,在振荡开始时的收缩力提供有关肢体刚度的信息。两种测试方法的原理都基于费尔德曼的λ模型。在一个为期6个月的MIR太空飞行中,对基于第二种方法的臂扩展器进行了探测。从负载振荡获得的结果证实,该设备非常适合捕获太空飞行引起的神经肌肉变化。

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