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Dynamics of A Vibration Isolation System Including Inertia of the Human BodyUsing an exercise device in a spacecraft is liable to transmit an unacceptable amount of vibration to that vehicle. This is commonly mitigated by a Vibration Isolation System (VIS), whose dynamics must be analyzed to confirm that the oscillatory forces on the spacecraft remain within allowed range, both from a structural and microgravity perspective (see, e.g., [1]). When modeling a VIS for countermeasures devices, one common approach is to record forces and moments applied on the floor while exercising, and then drive the VIS simulation by applying these recorded loads to the exercise platform part of the VIS mechanical model. This approach misses the fact that when exercising on a moving platform, the force and moment on it will differ from that on the stationary floor due to inertial effects involving the human body. For example, standing up on a platform as it gives under the subject’s feet reduces the foot force on it, and such inertial effects are especially complex for rotational motion.

In principle, one could model both the motion of the human body and dynamics of the VIS mechanism in a single combined simulation, e.g., employing a tool such as the commonly used biomechanical simulation OpenSim. Here, the joints of the human body would be driven kinematically along prescribed exercise trajectories while the dynamics engine computed the response of the VIS degrees of freedom. However, mechanism designers and biomechanics experts have their own established tools, making it very desirable to have a way of decoupling the biomechanics from the VIS modeling, simulation, and analyses. We have derived a set of equations that rigorously accomplishes this goal, and have implemented them as an interface function that provides an alternative driving mechanism for an existing force-based VIS analysis simulation. When enabled, the simulated human/VIS system dynamics is now driven by this function, instead of the recorded force methodology described above. The function is designed to accept input from a data file containing the required time-stamped human motion and inertia terms corresponding to the specific exercise in question. This data file is generated by an OpenSim plugin written for that purpose. The existing VIS analytical simulation is developed using NASA’s Trick Simulation Environment [2], as well as its MBDyn multibody dynamics [3] package.

The presentation will provide a detailed overview of the mathematical formulation, assumptions, plugin implementation, software interfaces, and results for a sample set of representative exercises. The results from this work aim to better inform VIS design efforts, as well as countermeasure device/protocol designs with respect to exercise type and frequency effects on vehicle structural and microgravity restrictions.
Document ID
20240007698
Acquisition Source
Johnson Space Center
Document Type
Poster
Authors
D. Frenkel
(CACI International (United States) Arlington, Virginia, United States)
R. K. Huffman
(METECS Houston, Texas, United States)
L. J. Quiocho
(Johnson Space Center Houston, United States)
K. H. Lostroscio
(Johnson Space Center Houston, United States)
Date Acquired
June 17, 2024
Subject Category
Physics (General)
Mathematical and Computer Sciences (General)
Report/Patent Number
Poster # 19261
Meeting Information
Meeting: NASA Human Research Program Investigator's Workshop (HRP IWS 2019)
Location: Galveston, TX
Country: US
Start Date: January 22, 2019
End Date: January 25, 2019
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 251546.06.15.05.01.72.03
CONTRACT_GRANT: NNJ14HA04B
CONTRACT_GRANT: NNJ14HA64B
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
External Peer Committee
Keywords
Countermeasures
Exercise
VIS
Modeling
Simulation
Biomechanics
EOMs
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