The fault detection and accommodation (FDA) methods that can be used for digital engine control systems are presently subjected to a flight test program in the case of the F-15 fighter's F100 engine electronic controls, inducing selected faults and then evaluating the resulting digital engine control responses. In general, flight test results were found to compare well with both ground tests and predictions. It is noted that the inducement of dual-pressure failures was not feasible, since FDA logic was not designed to accommodate them.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Fault detection and accommodation testing on an F100 engine in an F-15 airplane


    Beteiligte:
    Myers, L. P. (Autor:in) / Baer-Riedhart, J. L. (Autor:in) / Maxwell, M. D. (Autor:in)

    Erscheinungsdatum :

    1985-07-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Fault detection and accommodation testing on an F100 engine in an F-15 airplane

    MYERS, L. / BAER-RIEDHART, J. / MAXWELL, M. | AIAA | 1985


    Fault detection and accommodation testing on an F100 engine in an F-15 airplane

    Myers, L. P. / Baer-Riedhart, J. L. / Maxwell, M. D. | NTRS | 1985


    NASA Lewis F100 engine testing

    Werner, R. A. / Willoh, R. G., Jr. / Abdelwahab, M. | NTRS | 1984


    The F100 Engine

    Lancaster, Lanny T.G. / Eshbach, Russel E. | SAE Technical Papers | 1980


    Flight Research Using F100 Engine P680063 in the NASA F-15 Airplane

    Burcham, F. W. / Conners, T. R. / Maxwell, M. D. et al. | British Library Conference Proceedings | 1995