A computer simulation program package, IPIS (Interactive Parameter Identification System), which was developed at the NAL for evaluation of flight test techniques concerning determination of aircraft performance characteristics from measured data in dynamic maneuvers, is described. The system is composed of programs for determination of parametric nonlinear aerodynamic model using wind tunnel test data, flight simulation, measurement simulation, motion reconstruction, identification of nonlinear aerodynamic models and calculation of performance characteristics. The system was evaluated using a simulation for the NAL STOL airplane.


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    Title :

    Interactive Computer Program IPIS (Interactive Parameter Identification System) for Aircraft Parameter Identification


    Contributors:
    M. Nagayasu (author) / S. Sasa (author) / M. Yanagihara (author)

    Publication date :

    1988


    Size :

    45 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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