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Modeling the Impact of Space Suit Components and Anthropometry on the Center of Mass of a Seated Crewmember

机译:模拟航天服组件和人体测量学对坐式乘员的质心的影响

摘要

The Crew Impact Attenuation System (CIAS) is the energy-absorbing strut concept that dampens Orion Crew Exploration Vehicle (CEV) landing loads to levels sustainable by the crew. Significant COM variations across suited crew configurations would amplify the inertial effects of the pallet and potentially create unacceptable crew loading during launch and landing. The objective of this study was to obtain data needed for dynamic simulation models by quantifying the effects of posture, suit components, and the expected range of anthropometry on the COM of a seated individual. Several elements are required for the COM calculation of a suited human in a seated position: anthropometry, body segment mass, suit component mass, suit component location relative to the body, and joint angles defining the seated posture. Three-dimensional (3D) human body models, suit mass data, and vector calculus were utilized to compute the COM positions for 12 boundary manikins in two different seated postures. The analysis focused on two objectives: (1) quantify how much the wholebody COM varied from the smallest to largest subject and (2) quantify the effects of the suit components on the overall COM in each seat configuration. The location of the anterior-posterior COM varied across all boundary manikins by about 7 cm, and the vertical COM varied by approximately 9 to 10 cm. The mediolateral COM varied by 1.2 cm from the midline sagittal plane for both seat configurations. The suit components caused an anterior shift of the total COM by approximately 2 cm and a shift to the right along the mediolateral axis of 0.4 cm for both seat configurations. When the seat configuration was in the standard posture the suited vertical COM shifted inferiorly by as much as 1 cm, whereas in the CEV posture the vertical COM had no appreciable change. These general differences were due to the high proportion of suit mass located in the boots and lower legs and their corresponding distance from the body COM, as well as to the prevalence of suit components on the right side of the body.
机译:乘员撞击衰减系统(CIAS)是一种吸收能量的支柱概念,可将猎户座乘员探索车(CEV)的着陆负荷降低到机组人员可以承受的水平。在合适的乘员配置上,COM的显着变化会放大货盘的惯性效应,并可能在发射和降落期间造成不可接受的乘员负载。这项研究的目的是通过量化姿势,衣服组件以及人体测量学对坐着的人的COM的预期范围的影响来获得动态仿真模型所需的数据。在坐姿中,合适的人的COM计算需要几个要素:人体测量法,身体分段质量,衣服部件质量,衣服部件相对于身体的位置以及定义就座姿势的关节角度。利用三维(3D)人体模型,衣服质量数据和矢量演算来计算两种不同坐姿的12个边界人体模型的COM位置。分析着重于两个目标:(1)量化整个COM从最小到最大的变化量;(2)量化每个座椅配置中西服组件对整体COM的影响。前后COM的位置在所有边界人体模型上变化约7 cm,而垂直COM的变化约9至10 cm。两种座椅配置的中外侧COM与中线矢状平面相距1.2 cm。对于这两种座椅配置,防护服组件均导致总COM向前偏移约2 cm,并沿中外侧轴向右偏移0.4 cm。当座椅配置处于标准姿势时,合适的垂直COM向下偏移1 cm,而在CEV姿势下,垂直COM则没有明显变化。这些一般差异是由于位于靴子和小腿中的西服质量比例很高,以及它们与身体COM的对应距离,以及由于西服部件在身体右侧的普遍性。

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