US Army helicopters that will allow single-crewmember operability in tactical environments require a high degree of automation. A tightly integrated flight control and navigation system has been studied. An architecture is discussed which meets anticipated flight control and navigation requirements, at an acceptable weight, using techniques of functional and physical integration. The architecture maximizes the sharing of sensor and computational resources in a flight critical environment and uses modular equipment packaging, dual fault-tolerant tetrad ring-laser-gyro inertial measurement units, and triplex self-checking processor pair-based flight critical processing channels.<>


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    An advanced flight control and navigation system implementation for tactical helicopters


    Beteiligte:
    Bye, C.T. (Autor:in) / Bakken, J.T. (Autor:in)


    Erscheinungsdatum :

    01.07.1988


    Format / Umfang :

    424998 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Advanced Flight Control Technology Achievements at Boeing Helicopters

    K. H. Landis / C. Dabundo / J. M. Davis et al. | NTIS | 1995


    Advanced Flight Control Technology Achievements at Boeing Helicopters

    Landis, K. H. / Davis, J. M. / Dabundo, C. et al. | British Library Conference Proceedings | 1995


    Tactical information displays within battlefield helicopters

    Watts, A. / Silvester, C. / Society of British Aerospace Companies et al. | British Library Conference Proceedings | 1998