| 摘要 |
<p>PROBLEM TO BE SOLVED: To provide a missile guiding device capable of exerting excellent performance and mobility with the minimum required size without increasing the whole antenna in size and without losing the primary performance of a radar radio wave transmitting antenna and a command transmitting antenna respectively. SOLUTION: Multiple cross-dipole antennas 1-1 through 1-n are formed with multiple horizontal polarization dipoles 1-1-H through 1-n-H forming the horizontal polarization plane and multiple vertical polarization dipoles 1-1-V through 1-n-V forming the vertical polarization plane. Radar radio waves are transmitted from the horizontal polarization dipoles 1-1-H through 1-n-H in horizontal polarization, and command transmission radio waves are transmitted from the vertical polarization dipoles 1-1-V through 1-n-V in vertical polarization respectively. A beam controller 4 is provided, and the radar radio waves and the command transmission radio waves are prevented from being transmitted in the same direction at the same time by the beam controller 4.</p> |
