A piloted motion simulator evaluation, using the NASA Ames Vertical Motion Simulator, was conducted in support of a NASA Lewis Contractual study of the integration of flight and propulsion systems of a STOVL aircraft. Objectives of the study were to validate the Design Methods for Integrated Control Systems (DMICS) concept, to evaluate the handling qualities, and to assess control power usage. The E-7D ejector-augmentor STOVL fighter design served as the basis for the simulation. Handling-qualities ratings were obtained during precision hover and shipboard landing tasks. Handling-qualities ratings for these tasks ranged from satisfactory to adequate. Further improvement of the design process to fully validate the DMICS concept appears to be warranted.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Moving Base Simulation of an Integrated Flight and Propulsion Control System for an Ejector-Augmentor Stovl Aircraft in Hover


    Beteiligte:
    W. Mcneill (Autor:in) / W. W. Chung (Autor:in) / M. W. Stortz (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Integrated flight/propulsion control for supersonic STOVL aircraft

    Franklin, James A. / Stortz, Michael W. / Mihaloew, James R. | NTRS | 1990


    STOVL aircraft simulation for integrated flight and propulsion control research

    Mihaloew, James R. / Drummond, Colin K. | NTRS | 1989