Research on the Real-Time Simulation System Design for Missile Based on RT-LAB

Abstract

Abstract A semi-physical simulation system is developed based on the RT-LAB real-time simulation environment which is used to process simulation test of missile guidance controlling system. The system adopts design idea of modularization, development of all sub-system together and it integrates the Hi-fi missile aerodynamics environment, missile boron computer system, inertia measurement unit, high accurate aviation posture simulator, real missile boron port equipment, three-dimensional view and data backup system into one so that the performance of guidance controlling algorithm could be reflected comprehensively, directly and really. According to the comparison between test result of digital simulation and semi-physical system simulation, the feasibility of semi-physical simulation could be certified so that under the semi-physical simulation environment, more real and effective test could be checked for guidance controlling algorithm.