An analytic technique capable of predicting the landing characteristics of proposed aircraft configurations in the early stages of design was developed. In this analysis, a linear pilot-aircraft closed loop model was evaluated using experimental data generated with the NT-33 variable stability in-flight simulator. The pilot dynamics are modeled as inner and outer servo loop closures around aircraft pitch attitude, and altitude rate-of-change respectively. The landing flare maneuver is of particular interest as recent experience with military and other highly augmented vehicles shows this task to be relatively demanding, and potentially a critical design point. A unique feature of the pilot model is the incorporation of an internal model of the pilot's desired flight path for the flare maneuver.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Comparison of closed loop model with flight test results


    Beteiligte:
    George, F. L. (Autor:in)


    Erscheinungsdatum :

    1981-10-15


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Closed Loop IBC-System and Flight Test Results on the CH-53G Helicopter

    Furst, D. / Kesler, C. / Auspitzer, T. et al. | British Library Conference Proceedings | 2004


    Closed loop IBC results from CH-53G flight tests

    Arnold, Uwe T.P. / Fürst, Daniel | Elsevier | 2005


    JWST Cryo Fine Guidance Closed Loop Test Results

    Vila, M. Begoña / Lambros, Scott D. / Diaz, David M. et al. | NTRS | 2018


    OPEN LOOP FLIGHT TEST RESULTS AND CLOSED LOOP STATUS OF THE IBC SYSTEM ON THE CH-53G HELICOPTER

    Kessler, C. / Fuerst, D. / Arnold, U. T. P. et al. | British Library Conference Proceedings | 2003


    JWST Cryo Fine Guidance Closed Loop Test Results

    Vila, M. Begona / Lambros, Scott D. / Diaz, David M. et al. | NTRS | 2018