This paper describes an integrated approach to parametric diagnostics demonstrated in a flight control simulation of a space launch vehicle. The proposed diagnostic approach is able to detect incipient faults despite the natural masking properties of feedback in the guidance and control loops. Estimation of time varying fault parameters uses parametric vehicle-level data and detailed dynamical models. The algorithms explicitly utilize the knowledge of fault monotonicity (damage can only increase, never improve with time) where available. The developed algorithms can be applied to health management of next generation space systems. We present a simulation case study of rocket ascent application to illustrate and validate the proposed approach.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Integrated diagnostics of rocket flight control


    Contributors:
    Gorinevsky, D. (author) / Samar, S. (author) / Bain, J. (author) / Aaseng, G. (author)

    Published in:

    Publication date :

    2005


    Size :

    12 Seiten, 16 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Integrated diagnostics of rocket flight control

    Gorinevsky, D. / Samar, S. / Bain, J. et al. | IEEE | 2005


    Integrated Diagnostics of Rocket Flight Control

    Gorinevsky, D. / Samar, S. / Bain, J. et al. | British Library Conference Proceedings | 2005


    Overview of in-Flight Plume Diagnostics for Rocket Engines

    G. C. Madzsar / R. L. Bickford / D. B. Duncan | NTIS | 1992


    An overview of in-flight plume diagnostics for rocket engines

    Madzsar, G. C. / Bickford, R. L. / Duncan, D. B. | NTRS | 1992


    An overview of in-flight plume diagnostics for rocket engines

    MADZSAR, G. / BICKFORD, R. / DUNCAN, D. | AIAA | 1992