Modeling resonance characteristics of the Chang'e-7 lander modulated by solar panel rotation under lunar south-pole thermal environment

The Chang'e-7 (CE-7) mission will deploy the first seismometer at the lunar south pole to detect moonquakes and probe lunar interior structures in 2026 winter. However, the lander's vibration response to the extreme temperature cycles of the polar environment remains unclear, complicating the analysis of noise sources in seismic records. Here, we developed a high-fidelity finite-element model of the CE-7 lander to characterize its resonant behavior under the coupled influence of solar panel rotation and extreme thermal variations. Numerical results reveal that the lander's fundamental frequency (~0.76 Hz) at room temperature drifts significantly between 0.64 Hz and 0.87 Hz when the outside temperature varies from -180 to +80 °C. This frequency drift is primarily driven by thermally induced stiffness changes in the solar array supporting bracket, whereas geometric reconfiguration due to rotation plays a secondary role. Crucially, this resonance band directly overlaps with the primary seismic observation window (usually