Multivariable Control of Aeronautical Air Conditioning System Based on Thermal Comfort

2011-36-0129

10/04/2011

Authors Abstract
Content
It was purposed in this study the use of thermal comfort index as feedback parameter for multivariable control of aeronautical air conditioned system. Simulating the developed thermal model, the efficiency gain by using this control law was observed by comparing it with standard control models.
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Pages
11
Citation
Góes, L., and Gallo, E., "Multivariable Control of Aeronautical Air Conditioning System Based on Thermal Comfort," SAE Technical Paper 2011-36-0129, 2011, .
Additional Details
Publisher
Published
Oct 4, 2011
Product Code
2011-36-0129
Content Type
Technical Paper
Language
English