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Thermal Comfort Control of an Advanced Space Suit University of Missouri - Columbia

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Thornton, Samuel, author.
Conference Name:
31st International Conference On Environmental Systems (2001-07-09 : Orlando, Florida, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 2001
Summary:
This paper proposes an optimal control strategy for thermal comfort control of an advanced space suit. During an extravehicular activity (EVA), the astronaut's metabolic rate is time-varying depending on the working load, which would prescribe different reference skin temperatures. The purpose of thermal comfort control is to control the skin temperature to the reference value at a certain metabolic rate via a liquid cooling garment (LCG) for astronaut comfort. MPC is expected to achieve the control with the minimum consumable energy. After developing an operational definition of comfort, the structure of the controller and preliminary results are reported
Notes:
Vendor supplied data
Publisher Number:
2001-01-2268
Access Restriction:
Restricted for use by site license

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