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- W2077756923 abstract "When space vehicles reentry atmosphere at hypersonic speed, a plasma sheath enveloping the spacecraft forms. The plasma sheath is a medium which is frequency dependent and lossy, so reflection and attenuation will happen when radio signals transport through the plasma sheath. In this paper, Finite Difference Time Domain using Z-transform method(ZT-FDTD) is used to analyze the problem. At first, Maxwell equations are transformed to make the expression independent of the medium properties, thus, the same equations can be used in different frequency dependent mediums, this technology achieves the feature of code portability. Then the ZT-FDTD method is extended to the three-dimensional space, by comparing the sectional drawing of the result in 3D with that in 1D to make sure of the correctness of the simulation in 3D, and then the method is used to study the scattering characteristics of objects in different situations in 3D. Finally we compare and give the analysis of different situations." @default.
- W2077756923 created "2016-06-24" @default.
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- W2077756923 date "2009-12-11" @default.
- W2077756923 modified "2023-09-23" @default.
- W2077756923 title "Analysis for scattering of plasma sheath of aircraft by ZT-FDTD method in three-dimensional space" @default.
- W2077756923 doi "https://doi.org/10.1117/12.855174" @default.
- W2077756923 hasPublicationYear "2009" @default.
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