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    Modeling and Simulation Credibility Assessments of Musculoskeletal Computational Models for Simulating Astronaut Injuries Due to a Poor Spacesuit Fit

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    Date
    2024
    Author
    Gallo, Christopher A.
    Perkins, Richard A.
    Ivanoff, Athena E.
    Myers, Jerry G., Jr.
    Prabhu, Raj K.
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    Abstract
    The musculoskeletal (MS) system of astronauts is subject to physiological changes, potentially leading to injuries due to the exposure to different gravitational environments experienced during spaceflight. These injuries can occur while an astronaut is performing an extravehicular activity (EVA) in space, on lunar or planetary surfaces or while wearing a spacesuit during terrestrial training for an EVA. The opensim MS modeling software can assess EVA induced MS injury mechanisms such as muscle strains, ligament injuries, and joint injuries. One area of concern, since there are only a few different spacesuit sizes with limited adjustability, is the possibility of a poorly fitting spacesuit. This can cause unnatural joint motions and torques resulting in various MS injuries. A credibility assessment of the opensim modeling and simulation procedures is performed per NASA-STD-7009A to provide information on the credibility of the model's use in simulating EVA related injury mechanisms. The credibility assessment evaluated various opensim models against the following eight credibility factors: data pedigree, input pedigree, code verification, solution verification, conceptual validation, referent validation, results uncertainty, and results robustness (sensitivity). The models evaluated for EVA injuries will require additional credibility factor analysis and upgrades to the model features, such as adding ligaments to a whole-body model, to reliably predict and analyze the EVA injuries expected to occur due to a poor spacesuit fit. The degree of elevation strategy required to increase the credibility assessment scores will depend on the model complexity and the injury mechanism.
    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4305940
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