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.
Monte Carlo evaluation on implementation of autopilot in HIL simulation
01.01.2016
3089173 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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