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

TL;DR
This study models the Chang'e-7 lander's resonance behavior under lunar south-pole thermal conditions, revealing significant frequency drift caused by thermal and rotational effects, which impacts seismic data interpretation.
Contribution
Developed a high-fidelity finite-element model to analyze the lander's resonance characteristics influenced by thermal variations and solar panel rotation.
Findings
Fundamental frequency drifts from 0.64 Hz to 0.87 Hz with temperature changes.
Resonance band overlaps with primary seismic observation window.
Fundamental mode remains robust despite material uncertainties.
Abstract
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 {\deg}C. This frequency drift is primarily driven by thermally induced stiffness changes in the solar array supporting bracket, whereas geometric reconfiguration…
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Taxonomy
TopicsPlanetary Science and Exploration · Astro and Planetary Science · High-pressure geophysics and materials
