Sensitivity Analysis of Airdrop Condition Parameters Based on Response Surface Method
The airborne vehicle would suffer from impact at landing. The magnitude of impact and stability of airborne vehicle are constraint parameters of successful landing. There was a lack of scientific explanation on the sensitivity of landing condition parameters. For overcoming the deficiency of classic...
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| Veröffentlicht in: | Applied Mechanics and Materials 2014-06, Vol.565 (Aerospace and Mechanical Engineering), p.92-97 |
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| container_issue | Aerospace and Mechanical Engineering |
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| creator | Rui, Qiang Hong, Huang Jie Li, Jian Yang Wang, Hong Yan |
| description | The airborne vehicle would suffer from impact at landing. The magnitude of impact and stability of airborne vehicle are constraint parameters of successful landing. There was a lack of scientific explanation on the sensitivity of landing condition parameters. For overcoming the deficiency of classical sensitivity analysis, this paper describes the application of new technology for the sensitivity analysis. Based on the Finite Element and Response Surface method, the research on sensitivity analysis of landing condition parameters was proposed. The results have important significance in the design and optimization of airborne vehicle and airbags system. It can be also provide guidance for airdrop operation. |
| doi_str_mv | 10.4028/www.scientific.net/AMM.565.92 |
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| source | Scientific.net Journals |
| subjects | Airdrops Landing Landing conditions Mathematical analysis Optimization Response surfaces Sensitivity analysis Vehicles |
| title | Sensitivity Analysis of Airdrop Condition Parameters Based on Response Surface Method |
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