The invention relates to a COTM
satellite communication dual polarization quadruple ridged horn array antenna which is characterized in that 192 quadruple ridged horns are arranged at equal intervals in a square
regular array; an
azimuth plane comprises 32 columns, and a
pitch plane comprises 6 rows;
metal compensation grid plates are arranged at openings of the 192 quadruple ridged horns; each
metal compensation grid plate divides each quadruple ridged horn into four small equal
radiation units, so that the space of the 768 small
radiation units formed on an array plane is smaller than a wave length, and when constant-amplitude same-phase feeding occurs to the planes,
grating lobes cannot appear in a visible space, and the technical index requirements of the
International Telecommunication for access wide-angle sidelobe envelope can be met. According to the antenna
system, all technical indexes are advanced, the work is stable and reliable, the
insertion loss is low,
noise is little, and the antenna is provided with an ultrathin low profile and particularly suitable for being taken as a COTM
satellite communication antenna of a mini-automobile, and can be widely used in fields such as radars, communication,
remote sensing, remote measuring and the like.