A Mach/CAS control system using an elevator was designed and developed for use on the NASA TCV B737 aircraft to support research in profile descent procedures and approach energy management. The system was designed using linear analysis techniques primarily. The results were confirmed and the system validated at additional flight conditions using a nonlinear 737 aircraft simulation. All design requirements were satisfied.


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    Titel :

    Design and Verification by Nonlinear Simulation of a Mach/CAS Control Law for the NASA TCV B737 Aircraft


    Beteiligte:
    K. R. Bruce (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    68 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch