A method for determining a position of a doppler radar target in aircraft body coordinates is described. The panel can include a first face surface, a second face surface, a pair of opposing ends, a top surface, a bottom surface, and a shear wall wherein the first and second face surfaces are connected together. If so, the system will use the routing information in the client’s exception routing table to complete the call. The front bumper also has a pair of bumper apertures. The length decode unit may perform a length decode operation for each of the plurality of instruction bytes.