DocumentCode :
1932706
Title :
Variable Vector Countermeasure Suit (V2Suit) for Space Exploration
Author :
Duda, K.R. ; Newman, D.J.
Author_Institution :
Charles Stark Draper Lab., Inc., Cambridge, MA, USA
fYear :
2013
fDate :
2-9 March 2013
Firstpage :
1
Lastpage :
8
Abstract :
The “Variable Vector Countermeasure Suit (V2Suit) for Space Exploration” is an integrated countermeasure platform to mitigate the spaceflight-induced physiologic adaptation and de-conditioning that manifests during long-duration spaceflight and gravitational transitions. The V2Suit integrates flywheel gyroscopes and inertial measurement units within a wearable module that can be placed on the body segments, and when commanded in a coordinated manner provides a “viscous resistance” during movements. The system architecture, human-system integration, and three six degree-of-freedom simulations are presented which describe the magnitude and direction of the gyroscopic torque and resulting force within the module during representative arm movements. The results demonstrate of the ability of the V2Suit module design to generate a reaction force along a specified direction and reject perturbations due to body kinematics - collectively illustrating the feasibility of the concept.
Keywords :
aerospace; clothing; flywheels; gyroscopes; human factors; inertial systems; V2Suit; arm movement; body kinematics; body segment; coordinated manner; flywheel gyroscopes; gravitational transition; gyroscopic torque; inertial measurement units; integrated countermeasure platform; long-duration spaceflight; physiologic deconditioning; space exploration; space flight induced physiologic adaptation; variable vector countermeasure suit; viscous resistance; wearable module; Brain modeling; Coordinate measuring machines; Flywheels; Materials; Navigation; Physiology; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2013 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4673-1812-9
Type :
conf
DOI :
10.1109/AERO.2013.6496842
Filename :
6496842
Link To Document :
بازگشت