The invention relates to the technical field of
structural component testing, and specifically to a vibration state testing method and
system for
satellite solar wing assemblies, comprising: using a vibration testing
system to capture the wing edge and central axis vibration signals of each solar wing
assembly in real time; analyzing and extracting the edge
resonance signal of each
assembly and the
time series characteristics before reaching
resonance, as well as the central axis
resonance signal and the corresponding
time series variation characteristics; based on the
resonance signal samples and the corresponding
time series variation characteristics, in conjunction with resonance probability identification information, training a resonance monitoring module, and monitoring and warning the solar wing parallel
assembly, thereby solving the technical problem of being unable to identify and prevent potential
structural failure and performance loss of the solar wing assembly due to resonance in real time, and realizing the technical effect of accurately measuring the vibration characteristics of the solar wing parallel assembly, warning the potential resonance risk in advance, improving the overall
structural stability, and thus strengthening the refined management of the vibration behavior of the solar wing parallel assembly.