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Lumped Parameter Models of the Central Nervous System for VIIP ResearchINTRODUCTION: Current long-duration missions to the International Space Station and future exploration-class missions beyond low-Earth orbit, such as to Mars and asteroids, expose astronauts to increased risk of Visual Impairment and Intracranial Pressure (VIIP) syndrome [1]. It has been hypothesized that the headward shift of cerebral spinal fluid (CSF) and blood in microgravity may cause significant elevation of intracranial pressure (ICP), which in turn induces VIIP syndrome through biomechanical pathways [1, 2]. However, there is insufficient evidence to confirm this hypothesis. In this light, we are developing lumped-parameter models of fluid transport in the central nervous system (CNS) as a means to simulate the influence of microgravity on ICP. The CNS models will also be used in concert with the lumped parameter and finite element models of the eye described in the realted IWS abstracts submitted by Nelson et al., Feola et al. and Ethier et al. METHODS: We have developed a nine compartment CNS model (Figure 1) capable of both time-dependent and steady state fluid transport simulations, based on the works of Stevens et al. [3]. The breakdown of compartments within the model includes: vascular (3), CSF (2), brain (1) and extracranial (3). The boundary pressure in the Central Arteries [A] node is prescribed using an oscillating pressure function PA(t) simulating the carotid pulsatile pressure wave as developed by Linninger et al. [4]. For each time step, pressures are integrated through time using an adaptive-timestep 4th and 5th order Runga-Kutta solver. Once pressures are found, constitutive equations are used to solve for flowrates (Q) between each compartment. In addition to fluid flow between the different compartments, compliance (C) interactions between neighboring compartments are represented.
We are also developing a second CNS model based on the works of Linninger et al. [4] which takes a more granular approach to represent the interactions of the intracranial and spinal compartments with the inclusion of arteries, arterioles, capillaries, venules, veins, venous sinus, and ventricles. The flow through the arteries, veins and CSF compartments are governed by continuity, momentum and distensibility balance equations. Furthermore, unlike the Stevens et al. approach, the Monro-Kellie doctrine of constant cranial volume and the bi-phasic nature of the brain parenchyma are implemented. These features appear to be more consistent with the physiologic and anatomical behavior of the CNS, and follow a modeling philosophy similar to the lumped parameter eye model that is intended to be integrated with the CNS model. However, Linninger’s approach has never been implemented to include hydrostatic gradient and microgravity simulation capabilities. Therefore, we aim at implement this modeling approach for spaceflight simulations and assess its overall applicability to VIIP research. OBJECTIVES: We will present verification and validation test results for both models, as well as head-to-head comparison to explore their strengths and limitations with respect to mathematical implementation and physiological significance for VIIP research. In doing so, we hope to provide some guidance to the HRP research community on how to appropriately leverage lumped parameter models for space biomedical research.
Document ID
20140016929
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
Vera, J.
(NASA Glenn Research Center Cleveland, OH, United States)
Mulugeta, L.
(Universities Space Research Association Houston, TX, United States)
Nelson, E. S.
(NASA Glenn Research Center Cleveland, OH, United States)
Raykin, J.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Feola, A.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Gleason, R.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Samuels, B.
(Alabama Univ. Birmingham, AL, United States)
Myers, J. G.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
December 3, 2014
Publication Date
January 13, 2015
Subject Category
Numerical Analysis
Aerospace Medicine
Report/Patent Number
JSC-CN-32248
Meeting Information
Meeting: NASA Human Research Program Investigators'' Workshop
Location: Galveston, TX
Country: United States
Start Date: January 13, 2015
End Date: January 15, 2015
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Public Use Permitted.
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