표 2. | Table 2. 시뮬레이션 환경 | Simulation environment.
Objects
Incident wave
Observation
Fighter bi-static
θ
inc
=45°,
ϕ
inc
=0°
θ
=0°~360°,
ϕ
=0°
Tailless airplane bi-static
θ
inc
=120°,
ϕ
inc
=0°
θ
=0°~360°,
ϕ
=0°
Tailless airplane mono-static
θ
inc
=120°~240°,
ϕ
inc
=0°
Missile+ocean bi-static
θ
inc
=45°,
ϕ
inc
=0°
θ
=90°~−90°,
ϕ
=0°
Missile+ocean mono-static
θ
inc
=5°~60°,
ϕ
inc
=0°