A systematic analytical approach to the determination of helicopter IFR precision approach requirements is formulated. The approach is based upon the hypothesis that pilot acceptance level or opinion rating of a given system is inversely related to the degree of pilot involvement in the control task. A nonlinear simulation of the helicopter approach to landing task incorporating appropriate models for UH-1H aircraft, the environmental disturbances and the human pilot was developed as a tool for evaluating the pilot acceptance hypothesis. The simulated pilot model is generic in nature and includes analytical representation of the human information acquisition, processing, and control strategies. Simulation analyses in the flight director mode indicate that the pilot model used is reasonable. Results of the simulation are used to identify candidate pilot workload metrics and to test the well known performance-work-load relationship. A pilot acceptance analytical methodology is formulated as a basis for further investigation, development and validation.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Analytical methodology for determination of helicopter IFR precision approach requirements


    Beteiligte:
    Phatak, A. V. (Autor:in)

    Erscheinungsdatum :

    01.07.1980


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Helicopter Power Requirements

    Peyton Autry, C. | Emerald Group Publishing | 1946


    Analytical Approach to Helicopter-Ship Certification

    Min, Z. / Chang, C. / Siang, S. C. et al. | British Library Conference Proceedings | 2004


    Analytical Methodology, Test Methodology, and Requirements for Spaceflight Bellows

    Goyal, Vinay K. / Soltz, Brett / Sagrillo, Christopher N. et al. | AIAA | 2025


    Helicopter Inspection Design Requirements

    D. O. Blake / F. W. Hohn / F. E. Starses | NTIS | 1973