A new approach to the mechanization of the traditional navigation function can provide the key integration interface between the flight critical aircraft Fly-By-Wire stabilization and control and the remainder of the mission avionics. Redundant, integrated navigation and sensor assemblies provide all of the aircraft position, velocity, acceleration, angular rate, attitude, heading and air data states needed for both the flight control as well as the mission management functions. The architectural concept uses functional partitioning with distributed processing aimed at decoupling software dependencies between the various integrated avionics system elements.


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    Title :

    Helicopter avionics architecture for integrating flight critical functions


    Additional title:

    Architektur von Helikopteravionik fuer die Integration flugkritischer Funktionen


    Contributors:
    Osder, S.S. (author)


    Publication date :

    1986


    Size :

    8 Seiten, 8 Bilder, 1 Tabelle, 15 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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