Modeling resonance characteristics of the Chang'e-7 lander modulated by solar panel rotation under lunar south-pole thermal environment
This study establishes a high-fidelity finite-element model of the Chang'e-7 lander to demonstrate that extreme lunar south-pole thermal cycles, primarily affecting solar array stiffness, cause significant drift in the lander's fundamental resonance frequency (0.64–0.87 Hz), which critically overlaps with the seismic observation window and necessitates specific noise filtering strategies for accurate interior probing.