With a review of the capabilities and limitations of a modern digital aircraft flight control system, this paper considers the implications of the carriage and release of a wide range of stores for modern high performance military aircraft. The relevant vehicle characteristics are described by its aerodynamic, inertial, and structural properties which are all complex in their own right but are also substantially affected by stores carriage. This paper addresses the major issues involved and the interaction between stores integration and flight control system design for modern fighter aircraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Implications of Stores Carriage and Release for Aircraft Flight Control System Design


    Beteiligte:
    D. A. Allen (Autor:in) / K. F. Hulme (Autor:in)

    Erscheinungsdatum :

    1996


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    The Implications of Stores Carriage and Release for Aircraft Flight Control System Design

    Allen, D. A. / Hulme, K. F. / Advisory Group for Aerospace Research & Development | British Library Conference Proceedings | 1996




    Studies of Transonic Cavity Flows Relevant to Aircraft Stores Carriage and Release

    Knowles, K. / Lawson, N. J. / Bray, D. et al. | British Library Conference Proceedings | 2004


    Studies of Transonic Cavity Flows Relevant to Aircraft Stores Carriage and Release

    Knowles, K. / Lawson, N. J. / Bray, D. et al. | British Library Conference Proceedings | 2006