The flight test system described combines state-of-the-art microprocessor technology and high accuracy instrumentation with parameter identification technology which minimize data and flight time requirements. The system was designed to avoid permanent modifications of the test airplane and allow quick installation. It is capable of longitudinal and lateral-directional stability and control derivative estimation. Details of this system, calibration and flight test procedures, and the results of the Cessna 172 flight test program are presented. The system proved easy to install, simple to operate, and capable of accurate estimation of stability and control parameters in the Cessna 172 flight tests.


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    Titel :

    Development of a Simple, Self-Contained Flight Test Data Acquisition System


    Beteiligte:
    R. Clarke (Autor:in) / D. Shane (Autor:in) / J. Roskam (Autor:in) / D. I. Rummer (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    250 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Development of a simple, self-contained flight test data acquisition system

    Renz, R. R. L. / Clarke, R. / Mosser, M. A. et al. | NTRS | 1981


    Development of a simple, self-contained flight test data acquisition system

    Clarke, R. / Shane, D. / Roskam, J. et al. | NTRS | 1982




    Development of a Simple, Self-Contained Flight Test Data Acquisition System

    Rummer, Dale / Roskam, Jan / Mosser, Mark A. et al. | SAE Technical Papers | 1981