A real time digital simulation technique providing the capabilities needed to evaluate propulsion system performance and aircraft system interaction on NASA manned flight simulators, is discussed. A parameter correlation technique is used with real and pseudo dynamics in a stable integration convergence loop. The cycle time reported was 2.0 ms on one computer and 5.7 ms on the simulator computer. The model was found to be stable and accurate with time up to 50 ms. It is concluded that the program has generated a valuable simulation technology and flight simulator experience by providing an adequate level of detail to evaluate propulsion systems in a simulated flight environment.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A nonlinear propulsion system simulation technique for piloted simulators


    Contributors:

    Conference:

    Annual Pittsburgh Conference on Modelling and Simulation ; 1981 ; Pittsburgh, PA, US


    Publication date :

    1981-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English