A low cost flight test data acquisition system, applicable to general aviation airplanes, was developed which meets criteria for doing longitudinal and lateral stability analysis. Th package consists of (1) a microprocessor controller and data acquisition module; (2) a transducer module; and (3) a power supply module. The system is easy to install and occupies space in the cabin or baggage compartment of the airplane. All transducers are contained in these modules except the total pressure tube, static pressure air temperature transducer, and control position transducers. The NASA-developed MMLE program was placed on a microcomputer on which all data reduction is done. The flight testing program undertaken proved both the flight testing hardware and the data reduction method to be applicable to the current field of general aviation airplanes.


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    Titel :

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


    Beteiligte:
    R. R. L. Renz (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    208 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    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

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


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

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



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

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