The invention relates to a 
simulation analysis platform for thermally-induced micro-
vibration response of a 
satellite-borne flexible accessory, and belongs to the technical field of high-precision 
spacecraft design as well as 
dynamical simulation and control. The 
simulation analysis platform for thermally-induced micro-
vibration response of the 
satellite-borne flexible accessory comprises a data inputting and modeling module, an on-
orbit thermal analysis module, an equivalent 
thermal load derivation module, a high-precision 
modal analysis module, a high-precision 
vibration response analysis module and a post-
processing module, all of which are connected in a sequence; the output of the previous module serves as an input of the next module; and the analysis platform carries out analysis and 
simulation research on thermal vibration of an 
engineering-practical large-scale 
satellite-borne flexible accessory and research on corresponding 
software for calculation, and realizes the purpose of rapidly and efficiently obtaining the thermally-induced micro-vibration of large-scale flexible components and 
coupling vibration response between the components and a satellite. Meanwhile, the simulation analysis platform can promote 
engineering application, testing and 
verification of a 
thermal deformation and thermally-induced micro-vibration simulation technology of the large-scale satellite-borne flexible components, can drive progress of related support technical research and can accumulate a technological base for subsequent research of novel satellite types.