The Integrated Propulsion Control System (IPCS) demonstrates control of an entire supersonic propulsion module - inlet, engine afterburner, and nozzle - with an HDC 601 digital computer. The program encompasses the design, build, qualification, and flight testing of control modes, software, and hardware. The flight test vehicle is an F-111E airplane. The L.H. inlet and engine will be operated under control of a digital computer mounted in the weapons bay. A general description and the current status of the IPCS program are given.


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    Title :

    IPCS implications for future supersonic transport aircraft


    Contributors:
    Billig, L. O. (author) / Kniat, J. (author) / Schmidt, R. D. (author)


    Publication date :

    1976-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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