Performance Analysis and Optimization of a Bio-Inspired Spider-Web-Shaped Energy Absorbing Component for Legged Landers

Inspired by the structural characteristics of natural spider webs, a simplified configuration composed of multi-layer regular polygons was developed to design a novel energy absorbing component for legged landers. To investigate its compressive energy-absorption behavior, a parameterized finite element model (FEM) was established. By integrating optimized Latin hypercube experimental design with the FEM, the energy absorption characteristics under varying structural parameters were evaluated. Based on the FEM results, response surface methodology was employed to construct surrogate models that capture the mapping relationships between design parameters and performance indices. Using these surrogate models, the energy-absorbing component was optimized under three different ranges of average buffering force. Three optimized components with distinct average buffering forces were selected and connected in series, and their force–displacement responses during compression were computed through finite element simulations. The obtained response curves were incorporated into a multibody dynamics model of a Mars lander to verify performance, demonstrating that the lander can achieve effective soft landing.

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Publication Details

Journal
Machines
Published
2025-11-08
DOI
https://doi.org/10.3390/machines13111035
Primary Topic
Biomimetic flight and propulsion mechanisms
Type
article
Field-Weighted Citation Impact
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article

Performance Analysis and Optimization of a Bio-Inspired Spider-Web-Shaped Energy Absorbing Component for Legged Landers

Hui Wang, Kai Yang, Xueao Liu, Xuecong Wang et al.
Machines
Biomimetic flight and propulsion mechanisms
article

Performance Analysis and Optimization of a Bio-Inspired Spider-Web-Shaped Energy Absorbing Component for Legged Landers

Hui Wang, Kai Yang, Xueao Liu, Xuecong Wang, Kun Liu, Bin Zhang, Shiming Zhou
article en

Abstract

Inspired by the structural characteristics of natural spider webs, a simplified configuration composed of multi-layer regular polygons was developed to design a novel energy absorbing component for legged landers. To investigate its compressive energy-absorption behavior, a parameterized finite element model (FEM) was established. By integrating optimized Latin hypercube experimental design with the FEM, the energy absorption characteristics under varying structural parameters were evaluated. Based on the FEM results, response surface methodology was employed to construct surrogate models that capture the mapping relationships between design parameters and performance indices. Using these surrogate models, the energy-absorbing component was optimized under three different ranges of average buffering force. Three optimized components with distinct average buffering forces were selected and connected in series, and their force–displacement responses during compression were computed through finite element simulations. The obtained response curves were incorporated into a multibody dynamics model of a Mars lander to verify performance, demonstrating that the lander can achieve effective soft landing.

MachinesVol. 13(11)
North China University of Technology (CN), China Academy of Space Technology (CN), China Academy of Launch Vehicle Technology (CN), Beihang University (CN), University of Science and Technology Beijing (CN)
Openalex Percentile: Top 55%
Biomimetic flight and propulsion mechanisms
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