The semi-physical simulation of the guidance and control system has become an essential means in the missile development process, as it maximizes the replication of real flight environment characteristics in laboratory settings and enables comprehensive evaluation of the overall performance of missile guidance and control systems. With the accelerated development progress, the construction of the semi-physical simulation system also needs to be rapidly established. In the face of various non-standardized product requirements, it is of great significance to utilize generalized equipment resource modules for the rapid construction of HILS systems.