Optimized two panel aesa for aircraft applications

Optimized two panel aesa for aircraft applications

  • CN 104,145,192 A
  • Filed: 05/25/2012
  • Published: 11/12/2014
  • Est. Priority Date: 02/20/2012
  • Status: Active Application
First Claim
Patent Images

1. a radar system, comprising:

  • A pair of active electronic scanning array (AESA) flat board, this is separately positioned on the two opposite sides of central shaft to AESA flat board, wherein, the pointing direction of the one AESA flat board is setovered by a preset angles in a clockwise direction with respect to described central shaft, and the pointing direction of the 2nd AESA flat board is setovered counterclockwise to press described preset angles with respect to described central shaft;

    One controller, its respectively with this to the dull and stereotyped communication connection of each AESA in AESA flat board, this controller be configured selectively to carry out following at least one;

    Activate individually a described AESA flat board, so that the first overlay area on the first direction of being setovered by described central shaft to be provided,Activate individually described the 2nd AESA flat board, so that the second overlay area in the second direction of being setovered by described central shaft to be provided, orJointly activate this to AESA flat board, so that the 3rd overlay area between described the first overlay area and described the second overlay area to be provided.

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