Study on the Influence of Soil Parameters on the Cushioning Performance of Landing Airbags
Open Access
Abstract
To investigate the influence of soil parameters on the cushioning performance of landing airbags, a landing airbag cushioning dynamics model considering soil characteristics was established based on the control volume method and a crushable foam model. Experimental validation was conducted for both the airbag cushioning model and the soil impact model, respectively, with good consistency between simulated and experimental results. Based on the established model, the influence of soil on the cushioning performance of landing airbags was analyzed. The analysis results indicate that soil absorbs energy through compressive deformation during the cushioning process, thereby exhibiting a certain degree of cushioning performance. Softer soil absorbs more energy, and the payload is less prone to rebound. However, excessively soft soil causes the airbag to sink into the soil, hindering the venting of gas outward and resulting in hard landings for payloads. Therefore, three indicators—airbag peak pressure, payload maximum acceleration, and maximum drop height—are used to comprehensively evaluate the cushioning performance of airbags, and the influence laws of soil parameters are quantitatively researched. The research shows that the soil density, shear modulus, and yield parameters A1 and A2 significantly influence cushioning performance. Specifically, the shear modulus and yield parameter A1 exhibit logarithmic growth relationships with the three cushioning performance indicators, while the yield parameter A2 and soil density show linear growth relationships with the three cushioning performance indicators.Keywords
Funding Information
- Natural Science Foundation of Hunan Province (2025JJ80215)
- Hunan Provincial Major Science and Technology Research Project (2025QK2005)
- Hunan Province Key Research and Development Program Provincial and Municipal Joint Project (2024QY2009)
- Hunan Provincial Administration for Market Regulation Science and Technology Program Project (2024KJJH23)
- Xiangtan University Doctoral Research Start-Up Project (2023113101509)
This publication has 22 references indexed in Scilit:
- A review of the airbag landing system for spacecraftChinese Journal of Aeronautics, 2025
- Propulsion system integration on truss-braced aircraft: structural performance sensitivity to architectural design parametersAerospace Science and Technology, 2025
- Comprehensive crashworthiness simulation analysis of a large aircraft fuselage barrel section in various crash scenariosAerospace Science and Technology, 2024
- Test and numerical analysis for water entry of elastic cabin from amphibious aircraftAerospace Science and Technology, 2024
- Direct Folding Method of Cylindrical Airbag and Its Application in Landing BufferJournal of Aerospace Engineering, 2022
- DEM-FEM Coupling Analysis of Safe Landing of Reentry Capsule Considering Landing Attitude and Rebound ResponseJournal of Aerospace Engineering, 2021
- Optimal Design of Airbag Landing System without ReboundIOP Conference Series: Materials Science and Engineering, 2019
- Analysis on Characteristics of Structural Impact Response of Airborne Armored Vehicle in Landing ProcessIOP Conference Series: Materials Science and Engineering, 2019
- Finite element method simulation of explosive compaction in saturated loose sandy soilsSoil Dynamics and Earthquake Engineering, 2019
- Soil mechanics and plastic analysis or limit designQuarterly of Applied Mathematics, 1952