This paper deals with control of V/STOL aircraft in powered-lift flight. A review of representative operational mission tasks is presented for the take-off, transition, hover and landing flight phases. Characteristics inherent in the basic airframe and propulsion system and the behavior associated with control augmentation systems are considered. Demands for augmented stability and control response to meet certain mission operational requirements are discussed. Experience from ground-based simulation and flight experiments that illustrates the impact of augmented stability and control on aircraft design is related by example.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Control of V/STOL aircraft


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1986-05-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    STOL AIRCRAFT

    MOMBRINIE BRUNO | Europäisches Patentamt | 2020

    Freier Zugriff

    STOL AIRCRAFT

    MOMBRINIE BRUNO | Europäisches Patentamt | 2018

    Freier Zugriff

    STOL Aircraft

    NTRS | 1988


    STOL AIRCRAFT

    MOMBRINIE BRUNO | Europäisches Patentamt | 2020

    Freier Zugriff

    STOL aircraft

    MOMBRINIE BRUNO | Europäisches Patentamt | 2022

    Freier Zugriff