Sensitivity Analysis of Airdrop Condition Parameters Based on Response Surface Method

Jian Yang Li; Hong Yan Wang; Qiang Rui; Huang Jie Hong

doi:10.4028/www.scientific.net/AMM.565.92

Paper Titles

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Modeling of Atmospheric Processes Based on the Averaged Navier-Stokes Equations
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Exploration of Navigation Simulator Applying in Maritime Trial
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Estimation of Critical Performance Parameters of the Thermocouple in a Bypass Device, Made of SME Alloy, Designed for LIABs on Spacecraft
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Sensitivity Analysis of Airdrop Condition Parameters Based on Response Surface Method
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Quadrotor Position Control Using Cascaded Adaptive Integral Backstepping Controllers
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Asymmetrical Lateral Jet Interaction on a Slender Body in Supersonic Flow
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 565Sensitivity Analysis of Airdrop Condition...

Sensitivity Analysis of Airdrop Condition Parameters Based on Response Surface Method

Abstract:

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.

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Periodical:

Applied Mechanics and Materials (Volume 565)

Pages:

92-97

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.565.92

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Online since:

June 2014

Authors:

Jian Yang Li*, Hong Yan Wang, Qiang Rui, Huang Jie Hong

Keywords:

Airborne Vehicle, Airdrop Condition Parameters, Response Surface Method (RSM), Sensitivity Analysis

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* - Corresponding Author

References

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