The Open-Loop Onset Point (OLOP) criterion has, for many years, been successfully used as a method to predict quasi-non-linear pilot-induced oscillations (PIOs) for fixed-wing aircraft. Only limited research has been conducted using the criterion for prediction of PIOs occurring in rotorcraft. This paper details a study to extend the application of OLOP to rotorcraft, using the combination of control inputs appropriate for the task and a suitable pilot model. Results are compared between pilot subjective opinion and OLOP predictions, from tests performed in a ground-based simulation facility. Using ‘task-specific’ application of OLOP, results obtained in the investigation are encouraging, whereby the objective predictions reflect subjective pilot assessment. From results obtained, a modified boundary is presented.


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    Titel :

    The use of the Open-Loop Onset Point (OLOP) to predict rotorcraft pilot-induced oscillations


    Weitere Titelangaben:

    CEAS Aeronaut J


    Beteiligte:
    Jones, Michael (Autor:in)

    Erschienen in:

    CEAS Aeronautical Journal ; 11 , 3 ; 693-711


    Erscheinungsdatum :

    01.09.2020


    Format / Umfang :

    19 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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