An investigation of space suit mobility with applications to EVA operations
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001. === Includes bibliographical references (p. 193-196). === The primary aim of this thesis is to advance the current understanding of astronauts' capabilities and limitations in space-suited extra...
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ndltd-MIT-oai-dspace.mit.edu-1721.1-81052019-05-02T16:33:07Z An investigation of space suit mobility with applications to EVA operations Schmidt, Patricia Barrett, 1974- Dava J. Newman. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001. Includes bibliographical references (p. 193-196). The primary aim of this thesis is to advance the current understanding of astronauts' capabilities and limitations in space-suited extravehicular activity (EVA) by compiling a detailed database of the torques needed to bend the joints of a space suit, developing models of the mechanics of space suit joints based on experimental data, and utilizing these models to estimate a human factors performance metric, the work envelope for space suited EVA work. A detailed space suit joint torque-angle database is compiled in a novel experimental approach that uses space-suited human test subjects to generate realistic, multi-joint motions, which are used to drive an instrumented robot to measure the torques required to accomplish the motions in a pressurized space suit. Based on the experimental data, a mathematical model using the Preisach hysteresis modeling technique is developed to predict joint torque from the joint angle history. Two physics-based models describing the bending load-deflection characteristics of pressurized fabric cylinders were compared to the experimental space suit data. The beam model assumes that bending deflections are completely attributable to elongation of the fabric cylinder wall, while the membrane model assumes that the fabric never stretches. (cont.) The experimental data corresponds closely with the membrane model, implying that space suit joint stiffness is primarily determined by volume changes as the joint bends and the resulting compression of the gas inside the space suit. The space suit models were applied in a computational work envelope analysis to determine the volume in which a space-suited astronaut can comfortably work. A new method that uses inverse kinematics and the space suit model to calculate a work envelope based on visibility constraints and human strength limits is developed. Sensitivity analysis of the work envelope indicates that improving shoulder mobility and upward and downward visibility enlarge the space-suited work envelope. by Patricia Barrett Schmidt. Ph.D. 2005-08-24T20:22:33Z 2005-08-24T20:22:33Z 2001 2001 Thesis http://hdl.handle.net/1721.1/8105 51284116 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 254 p. 19373230 bytes 19372987 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology |
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Aeronautics and Astronautics. |
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Aeronautics and Astronautics. Schmidt, Patricia Barrett, 1974- An investigation of space suit mobility with applications to EVA operations |
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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001. === Includes bibliographical references (p. 193-196). === The primary aim of this thesis is to advance the current understanding of astronauts' capabilities and limitations in space-suited extravehicular activity (EVA) by compiling a detailed database of the torques needed to bend the joints of a space suit, developing models of the mechanics of space suit joints based on experimental data, and utilizing these models to estimate a human factors performance metric, the work envelope for space suited EVA work. A detailed space suit joint torque-angle database is compiled in a novel experimental approach that uses space-suited human test subjects to generate realistic, multi-joint motions, which are used to drive an instrumented robot to measure the torques required to accomplish the motions in a pressurized space suit. Based on the experimental data, a mathematical model using the Preisach hysteresis modeling technique is developed to predict joint torque from the joint angle history. Two physics-based models describing the bending load-deflection characteristics of pressurized fabric cylinders were compared to the experimental space suit data. The beam model assumes that bending deflections are completely attributable to elongation of the fabric cylinder wall, while the membrane model assumes that the fabric never stretches. === (cont.) The experimental data corresponds closely with the membrane model, implying that space suit joint stiffness is primarily determined by volume changes as the joint bends and the resulting compression of the gas inside the space suit. The space suit models were applied in a computational work envelope analysis to determine the volume in which a space-suited astronaut can comfortably work. A new method that uses inverse kinematics and the space suit model to calculate a work envelope based on visibility constraints and human strength limits is developed. Sensitivity analysis of the work envelope indicates that improving shoulder mobility and upward and downward visibility enlarge the space-suited work envelope. === by Patricia Barrett Schmidt. === Ph.D. |
author2 |
Dava J. Newman. |
author_facet |
Dava J. Newman. Schmidt, Patricia Barrett, 1974- |
author |
Schmidt, Patricia Barrett, 1974- |
author_sort |
Schmidt, Patricia Barrett, 1974- |
title |
An investigation of space suit mobility with applications to EVA operations |
title_short |
An investigation of space suit mobility with applications to EVA operations |
title_full |
An investigation of space suit mobility with applications to EVA operations |
title_fullStr |
An investigation of space suit mobility with applications to EVA operations |
title_full_unstemmed |
An investigation of space suit mobility with applications to EVA operations |
title_sort |
investigation of space suit mobility with applications to eva operations |
publisher |
Massachusetts Institute of Technology |
publishDate |
2005 |
url |
http://hdl.handle.net/1721.1/8105 |
work_keys_str_mv |
AT schmidtpatriciabarrett1974 aninvestigationofspacesuitmobilitywithapplicationstoevaoperations AT schmidtpatriciabarrett1974 investigationofspacesuitmobilitywithapplicationstoevaoperations |
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1719042836848967680 |