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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Simulation Study of Space Suit Thermal Control


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    International Conference On Environmental Systems ; 2000



    Publication date :

    2000-07-10




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Space Suit Thermal Dynamics

    Campbell, Anthony B. / Nair, Satish S. / Miles, John B. et al. | NTRS | 1998


    Space Suit Thermal Dynamics

    A. B. Campbell / S. S. Nair / J. B. Miles et al. | NTIS | 1998


    Extravehicular space suit thermal insulations

    FRENCH, B. / RICHARDSON, D. / RUCCIA, F. | AIAA | 1970



    Space Suit

    NTIS | 1994