Table 4 RCS indicator of the aircraft in Z1 mode, α = 0° ~ 360°, fRH = 6 GHz, ωr1 = ωr2 = 0.3142 rad/s, Am1 = Am2 = 0°.
From: Z-folding aircraft electromagnetic scattering analysis based on hybrid grid matrix transformation
t (s) | β = 0° | β = 10° | ||||
|---|---|---|---|---|---|---|
0.667 | 2.444 | 3.630 | 0.667 | 3.185 | 4.0 | |
Mean (dBm2) | 15.5527 | 15.7285 | 16.0027 | 7.3727 | 6.2272 | 12.8321 |
Peak (dBm2) | 39.2094 | 39.7478 | 39.8298 | 32.1615 | 28.6215 | 37.9374 |
