Table 5 RCS indicator of the aircraft, β = 0°, fRH = 6 GHz, ωm1 = ωm2 = 0.1963 rad/s, t = 0 ~ 4.407 s.

From: Z-folding aircraft electromagnetic scattering analysis based on hybrid grid matrix transformation

α (°)

10

20

30

80

90

100

Mean (dBm2)

− 6.6604

− 13.5478

− 14.5690

− 5.6471

30.7186

− 0.0831

Peak (dBm2)

− 1.9564

− 7.3101

− 6.2955

0.7757

45.8095

5.6211

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