STOLAND has been developed to perform navigation, guidance, control, and flight management experiments in advanced V/STOL aircraft. An integrated digital concept using modern avionics components was selected as the simplest approach to maximizing versatility and growth potential. Unique flexibility has been obtained by use of a single, general-purpose digital computer for all navigation, guidance, control, and displays computation. Modularity of the software insures easy change of experiments. The general-purpose computer is integrated with flexible pilot controls and with both electromechanical and CRT displays for maximum cockpit versatility. A complex hierarchy of control modes with safety monitors and interlocks has been provided.


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    Titel :

    Development of STOLAND, a versatile navigation, guidance and control system.


    Beteiligte:
    Hansen, Q. M. (Autor:in) / Young, L. S. (Autor:in) / Rouse, W. E. (Autor:in) / Osder, S. S. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aircraft Design, Flight Test, and Operations Meeting ; 1972 ; Los Angeles, CA


    Erscheinungsdatum :

    1972-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Development of STOLAND, a versatile navigation, guidance and control system

    Young, L. S. / Hansen, Q. M. / Rouse, W. E. et al. | NTRS | 1972



    Development of Stoland, a Versatile Navigation, Guidance and Control System

    L. S. Young / Q. M. Hansen / W. E. Rouse et al. | NTIS | 1972


    V/STOLAND avionics system flight-test data on a UH-1H helicopter

    Baker, F. A. / Jaynes, D. N. / Corliss, L. D. et al. | NTRS | 1980