A simulation framework of a guided ballistic missile has been developed to aid the design and development of autopilot of a missile guidance system. In this framework, a hardware-in-the-loop (HIL) is utilized in the autopilot. The system dynamic engine works with the hardware autopilot in order to guide the simulated missile platform during a flight. Performance of the hardware autopilot is evaluated based on the Circular Error Probability (CEP) of the impact points obtained from a Monte-Carlo experiment. Results are compared against CEP of simulation outputs from both unguided flights and guided flights with software autopilot.


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    Title :

    Monte Carlo evaluation on implementation of autopilot in HIL simulation


    Contributors:


    Publication date :

    2016-01-01


    Size :

    3089173 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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