Simulation of spacecraft battery operation is implemented. Robust design experiment to obtain optimum battery operational parameters is performed. It is found that short term tests using robust design of experiments can provide guidelines for optimum battery operation. It is decided to use robust design approach to provide guidelines for battery operation on current spacecraft in orbit as batteries age (GRO, UARS, EUVE, TOPEX).


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    NASA battery testbed: A designed experiment for the optimization of LEO battery operational parameters


    Contributors:


    Publication date :

    1996-02-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    NASA Battery Testbed: A Designed Experiment for the Optimization of LEO Battery Operational Parameters

    Deligiannis, F. / Perrone, D. / DiStefano, S. et al. | British Library Conference Proceedings | 1996


    NASA Battery Testbed Capabilities and Results

    Deligiannis, F. / Di Stefano, S. / Perrone, D. et al. | British Library Conference Proceedings | 1995


    Design of a Nickel-Hydrogen Battery Simulator for the NASA EOS Testbed

    Patil, Ashok R. / Cho, Bo H. / Sable, Dan M. et al. | SAE Technical Papers | 1992


    NASA Electrified Aircraft Testbed (NEAT)

    Jankovsky, Amy / Haglage, Joe | NTRS | 2020


    NASA Telescience Testbed Pilot Program

    Leiner, B. M. | NTRS | 1989