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Feasibility of Earthbound Motion in Lunar GravityBACKGROUND: Marginal stability of astronaut movement while performing lunar surface tasks has been well documented, and is clearly demonstrated in videos of falls, and near falls, during Apollo Lunar Extravehicular Activities. Referencing mission reports from Apollo 15 and 16 [1, 2], suspected causes for falls include: surface conditions, visibility, and gravitational effects (hypogravity). In this preliminary test, we employ the open-source biomechanical tool OpenSim [3, 4] to analyze the impact of lunar gravity (Lg) on two object-pickup motions performed by a single shirt-sleeved subject. Specifically, we attempt to answer the following questions based on an estimation of the Center of Mass Projection (CoMP) and ground reaction force Center of Pressure (COP) as it relates to the astronaut Base of Support (BOS) for 1g and Lg conditions:
1. Is the task motion, as performed in 1g, dynamically feasible in 1g and Lg?
2. Can we make the motion dynamically feasible in Lg by slowing it down?
3. Is the Lg COP equal to the 1g COP at a theoretically predicted reduction in motion speed?

METHODS AND RESULTS: To answer the first question, the gravitational acceleration in the OpenSim model is modified from a nominal 9.81 m/s2 to 1.64 m/s2, and the 1g joint trajectory is input to an OpenSim based method [5] for estimating ground reaction forces and moments. From this method, the position of the CoMP and COP can be estimated and checked to see if they remain within a simulated BOS formed from the footprint of the OpenSim model to determine whether the motion is dynamically feasible. As expected, both of the motions were estimated to be feasible in a 1g environment, however, both motions had periods of infeasibility in Lg.

It is well known that crew members make adjustments to motion trajectories in altered gravity fields to maintain balance. As a first step, we considered the simple adjustment of slowing the motion in Lg by a constant factor. This was accomplished by scaling the time stamps in the motion trajectory file by that factor. For the two motions considered, it was found that scale factors of 1.3 and 1.4 kept the COP just within the subject BOS. The CoMP is unchanged by the gravity field. Simple analysis of an inverted pendulum in the Lg environment, which generalizes to a general multibody system, leads to a theoretical prediction that a reduction in speed factor of √1g/Lg, or 2.445, will make the COP trajectory in Lg equivalent to that in 1g. When the above procedure was performed with a factor of 2.445, the estimated COP in Lg, was observed to be very close to that in 1g.

In summary, we have developed a method for estimating the CoMP and COP in Lg, for subject motion collected in 1g. We believe this method can prove to be a valuable check and balance for simulated Lg training and testing by exposing potential simulator-induced artifacts that make the simulated task motion seem possible, when in fact, it would violate the above criteria. We also note that a reduction in task speed should tend the task motion towards stability, with a theoretical slowdown factor of √1g/Lg making the motion stability equal to that in 1g according to the CoMP and COP criteria.
Document ID
20205008578
Acquisition Source
Johnson Space Center
Document Type
Abstract
Authors
R K Huffman
(METECS Houston, Texas, United States)
D Frenkel
(CACI International (United States) Arlington, Virginia, United States)
C A Bell
(CACI International (United States) Arlington, Virginia, United States)
K H Lostroscio
(Johnson Space Center Houston, Texas, United States)
L J Quiocho
(Johnson Space Center Houston, Texas, United States)
Date Acquired
October 13, 2020
Publication Date
February 1, 2021
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Man/System Technology and Life Support
Meeting Information
Meeting: NASA Human Research Program Investigators' Workshop (HRP IWS)
Location: Virtual
Country: US
Start Date: February 1, 2021
End Date: February 4, 2021
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
CONTRACT_GRANT: NNJ14HA64B
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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