The present work deals with the investigation of longitudinal aircraft stability derivative coefficients using flight trials. A longitudinal model is predicted using semi-empirical models. The most important stability derivatives are identified with a time-domain approach, whereas the macroscopic dynamic characteristics, e.g. the short period mode, are also verified with an independent frequency-domain technique. The activity shows how the aerodynamic model evaluation can be also trickier for a conventional aft-tail ultra-light aircraft.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Identification of Longitudinal Aircraft Modes and Aerodynamic Parameters with Flight Trials


    Contributors:


    Publication date :

    2024-06-03


    Size :

    783496 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English