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 |