Several YF-12C airplane analog control systems were converted to a digital system. Included were the air data computer, autopilot, inlet control system, and autothrottle systems. This conversion was performed to allow assessment of digital technology applications to supersonic cruise aircraft. The digital system was composed of a digital computer and specialized interface unit. A large scale mathematical simulation of the airplane was used for integration testing and software checkout.


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    Title :

    YF-12 Cooperative Airframe/Propulsion Control System Program, Volume 1


    Contributors:
    D. L. Anderson (author) / G. F. Connolly (author) / F. M. Mauro (author) / P. J. Reukauf (author) / R. Marks (author)

    Publication date :

    1980


    Size :

    120 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    YF-12 cooperative airframe/propulsion control system program, volume 1

    Anderson, D. L. / Connolly, G. F. / Mauro, F. M. et al. | NTRS | 1980


    Cooperative Airframe/Propulsion Control for Supersonic Cruise Aircraft

    Berry, Donald T. / Schweikhard, William G. | SAE Technical Papers | 1974


    Cooperative airframe/propulsion control for supersonic cruise aircraft

    Schweikhard, W. G. / Berry, D. T. | NTRS | 1974


    The Integrated Airframe/Propulsion Control System Architecture Program (IAPSA)

    Daniel L Palumbo / Gerald C Cohen / Charles W Meissner | NTRS | 1990


    Integrated Airframe Propulsion Control

    R. E. Fennell / S. B. Black | NTIS | 1982