Discrete element modeling of JLU-H lunar highland simulant
In order to accurately model the machine-lunar soil simulant interaction, this study combined physical and simulation experiments to calibrate the discrete element simulation parameters of the JLU-H lunar highland simulant. First, the intrinsic parameters and the true angle of repose of the JLU-H were determined through physical tests to provide data for subsequent simulation tests. A Plackett-Burman test was designed to identify and select the parameters that have a significant effect on the angle of repose. The range of values of the significant parameters was then optimized using the steepest climb test. The Box-Behnken test was then utilized to calibrate and obtain the optimal parameter combinations. Finally, a validation test of the angle of repose was conducted using the calibrated DEM parameters. The relative error between the simulation results and the test results was 1.54 %. Then further straight shear tests were conducted to verify the accuracy and validity of the DEM parameters. The results show that the calibrated parameters can provide a reference for the selection of discrete element simulation parameters for lunar soil simulant and the design and optimization of drilling and excavation machinery for lunar exploration .
Authors
- Xumin Sun
- Rui Zhang (ORCID: https://orcid.org/0000-0001-7354-0997)
- Zhenyu Hu (ORCID: https://orcid.org/0000-0003-1403-1732)
- Meng Zou (ORCID: https://orcid.org/0000-0003-0498-4791)
- Hua Zhang (ORCID: https://orcid.org/0000-0003-4326-7875)
- Weijun Wang
Institutions
- Jilin University (CN)
Publication Details
- Journal
- Advances in Space Research
- Published
- 2024-09-19
- DOI
- https://doi.org/10.1016/j.asr.2024.09.031
- Citations
- 1
- Primary Topic
- Soil Mechanics and Vehicle Dynamics
- Type
- article
- Field-Weighted Citation Impact
- 0.26