Table 7 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

70

80

90

Mean (dBm2)

− 6.5051

− 12.5186

− 18.4253

− 12.0001

− 5.0794

28.0423

Peak (dBm2)

− 2.1126

− 7.6584

− 11.1492

− 5.1155

1.6669

43.0769