The invention discloses a batch automatic extraction method and
system for
satellite stand-alone dynamics finite element results, relates to the technical field of
satellite structure finite elements, and aims to solve the problems that
manual extraction of the
satellite stand-alone dynamics finite element results is huge in
workload and prone to result errors at present. Preprocessing the single-
machine geometric model, the single-
machine matching table, the whole-satellite
assembly model, the finite
element model and the first solving file respectively; based on the single
machine matching table, after single machine installation point coordinates in the whole satellite
assembly model are extracted, a single machine geometric model installation point coordinate table is exported; based on the first solving file, the stand-alone geometric model installation point coordinate table and the stand-alone geometric model installation points, generating a finite
element model installation point node table corresponding to the stand-alone geometric model installation point coordinate table, and outputting a second solving file; and based on the finite
element model installation point node table and the second solving file, generating a result, enabling the result to correspond to the single machine, and outputting a chart result.