Practical aspects of identifying dynamic models for aircraft in real time were studied. Topics include formulation of an equation-error method in the frequency domain to estimate non-dimensional stability and control derivatives in real time, data information content for accurate modeling results, and data information management techniques such as data forgetting, incorporating prior information, and optimized excitation. Real-time dynamic modeling was applied to simulation data and flight test data from a modified F-15B fighter aircraft, and to operational flight data from a subscale jet transport aircraft. Estimated parameter standard errors and comparisons with results from a batch output-error method in the time domain were used to demonstrate the accuracy of the identified real-time models.


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    Titel :

    Real-Time Dynamic Modeling - Data Information Requirements and Flight Test Results


    Beteiligte:

    Kongress:

    AIAA Atmospheric Flight Mechanics Conference ; 2008 ; Honolulu, HI, United States


    Erscheinungsdatum :

    2008-08-18


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Real-Time Dynamic Modeling: Data Information Requirements and Flight Test Results

    Morelli, E. / Smith, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008