Abstract: A semiconductor wafer is provided including: processing cores; and die structures each including at least one processing core. Each processing core includes a set of first input output (I/O) interfaces configured for communication between the processing core and a second processing core, wherein the processing core and the second processing core are included in a first die structure of the die structures. Each processing core includes a second input output (I/O) interface configured for communication between the processing core and a third processing core, wherein the third processing core is included in a second die structure of the die structures. The processing cores are spaced apart by a target distance associated with separating one or more processing cores or one or more die structures from the semiconductor wafer.

Abstract: A method of compensating for atmospheric effects to detect the actual location of low elevation objects using near horizon radar to detect an object which utilizes a preexisting satellite structured to send a signal indicating the position and velocity of said satellite, wherein the location of the satellite is known. The method includes a step of providing a radar site, a first receiver structured to receive a signal from the satellite indicating an apparent location of the satellite, and a second receiver, located at a distance from the radar site, structured to receive the satellite signal and which indicates the observed location of the satellite. The first receiver is utilized to receive a signal from the satellite when the satellite is at a low elevation. This signal indicates the apparent location and velocity of the satellite.