This application provides an
intelligent control method and device for airborne
test equipment, applied in the field of airborne test technology. It includes: acquiring the status information of multiple airborne test devices within a preset time period; sampling and extracting features from the status information of each airborne test device to obtain initial physical quantities; mapping the initial physical quantities from a two-dimensional space to a target dimension space to construct target feature parameters, wherein the dimension of the target dimension space is higher than that of the two-dimensional space and the target feature parameters include at least nonlinear terms and / or interaction terms constructed from the initial physical quantities; and determining the current operating status of the airborne
test equipment based on the positional relationship between the target feature parameters and a preset decision hyperplane. This significantly simplifies the cumbersome process of manually switching and checking each interface individually, greatly shortens pre-flight preparation time, effectively supports the mission requirements of multiple remote simultaneous launches, and effectively avoids flight mission failures caused by hidden faults.