The F-117A night attack aircraft flight management system (FMS) is described. The need for and purpose of the system are described, and the design goals are identified. The various modes and their important features are presented. The pitch and speed control laws are shown.<>


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    Titel :

    Flight management system of the F-117A


    Beteiligte:
    Combs, S.R. (Autor:in) / Loschke, R.C. (Autor:in) / Tauke, G.J. (Autor:in)


    Erscheinungsdatum :

    01.07.1992


    Format / Umfang :

    571838 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    F-117A

    Online Contents | 1997


    F-117A Composite Rudder Aeroelastic Stability Flight Test Program

    Green, S. / Fernandez, D. / AIAA | British Library Conference Proceedings | 1994


    The F-117A "Nighthawk"

    Lidh, R. D. / Society of Allied Weight Engineers | British Library Conference Proceedings | 1992



    Dynamic Inversion Applied to the F-117A

    Colgren, R. / Enns, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1997