The philosophy and techniques adopted for the flight testing of the swing-wing Tornado aircraft digitally based self-contained all-weather NAV/ATTACK avionics system are presented. The subsystems for navigation, displays, flight control, weapon aiming, computing, and data transmission are described. The development organization and development program system are described briefly. The stage 3 flight trials program is detailed.


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    Title :

    The Philosophy Adopted for the Flight Testing of the Panavia Tornado Avionics System in Hack Aircraft


    Contributors:

    Publication date :

    1977


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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