Automatic thermal comfort control for the minimum consumables PLSS is undertaken using several control approaches. Accuracy and performance of the strategies using feedforward, feedback, and gain scheduling are evaluated through simulation, highlighting their advantages and limitations. Implementation issues, consumable usage, and the provision for the extension of these control strategies to the cryogenic PLSS are addressed.
Simulation Study of Space Suit Thermal Control
Sae Technical Papers
International Conference On Environmental Systems ; 2000
2000-07-10
Conference paper
English
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