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Influence of hypersonic turbulence in plasma sheath on synthetic aperture radar imaging
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On the basis of the fractal theory and measurements of hypersonic turbulence, the spectral index, and two‐dimensional (2D) power spectrum of the refractive index fluctuation are derived, and the 2D band‐limited Weierstrass fractal function is applied to simulate the refractive index fluctuation in hypersonic turbulence. Thus, the impact of hypersonic turbulence on synthetic aperture radar (SAR) imaging system is simulated using the fractal phase screen method. Results show that the resolution of SAR imaging is severely deteriorated under the influence of hypersonic turbulence. The phase error caused by the turbulence microstructures in the plasma sheath becomes more apparent with the increase in the fractal dimension of the hypersonic turbulence. The larger Reynolds number associated with the hypersonic turbulence results in a more evident microstructure fluctuation and inferior imaging quality. Furthermore, when an aircraft flies at high speed, the azimuth focus is considerably sensitive to the turbulence microstructure along the direction of flow field. Consequently, hypersonic turbulence in the plasma sheath has a significantly larger effect on the azimuth than on the range in point‐target imaging.
Institution of Engineering and Technology (IET)
Title: Influence of hypersonic turbulence in plasma sheath on synthetic aperture radar imaging
Description:
On the basis of the fractal theory and measurements of hypersonic turbulence, the spectral index, and two‐dimensional (2D) power spectrum of the refractive index fluctuation are derived, and the 2D band‐limited Weierstrass fractal function is applied to simulate the refractive index fluctuation in hypersonic turbulence.
Thus, the impact of hypersonic turbulence on synthetic aperture radar (SAR) imaging system is simulated using the fractal phase screen method.
Results show that the resolution of SAR imaging is severely deteriorated under the influence of hypersonic turbulence.
The phase error caused by the turbulence microstructures in the plasma sheath becomes more apparent with the increase in the fractal dimension of the hypersonic turbulence.
The larger Reynolds number associated with the hypersonic turbulence results in a more evident microstructure fluctuation and inferior imaging quality.
Furthermore, when an aircraft flies at high speed, the azimuth focus is considerably sensitive to the turbulence microstructure along the direction of flow field.
Consequently, hypersonic turbulence in the plasma sheath has a significantly larger effect on the azimuth than on the range in point‐target imaging.
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