This thread has been locked.

If you have a related question, please click the "Ask a related question" button in the top right corner. The newly created question will be automatically linked to this question.

CCS/IWR1642: IWR1642 Bifurcation Sag in Pitch Plane

Part Number: IWR1642

Tool/software: Code Composer Studio

Hello TI engineers, we are using IWR1642 to test the elevation pattern. The radar board is designed by ourselves. The chip uses IWR1642, but when we test the elevation pattern, we have a score of -10 °. What is the cause of the fork depression? When we designed the antenna, there were two columns of virtual arrays on both sides of the TX0 and TX1 transmitting antennas. After we tried to remove the virtual array, the position of the bifurcation moved from -10 ° to -3 °. What could cause the bifurcation of our elevation? Below is a picture of our elevation pattern. thank you very much.