Guided missile calibration method

摘要

A method for calibrating the radar system includes the steps of: replacing stored statistically generated "average" error correction coefficients with error correction coefficients personal to a missile under test. More particularly, stored in the missile's memory are: (a) first personalized error correction coefficients generated in response to test signals produced internal to the missile and injected into a monopulse arithmetic unit for the missile's receiver/processor; and (b) a second set of personalized error coefficients generated in response to test signals external to the missile and injected through the missile's antenna to the receiver/processor. The missile includes a radio frequency (R.F.) energy test signal generator for performing a test during the missile's flight to determine "in-flight" personalized error correction coefficients. The test is performed in-flight by injecting the R.F. energy test signal generated internal to the missile during the missile's flight into the monopulse arithmetic unit for the receiver/processor. The receiver/processor: (a) compares the first set of error correction coefficients with the "in-flight" error coefficients and adjusts the second set of error correction coefficients in accordance with such comparison; and, (b) if R.F. energy external to the missile is less than a predetermined threshold level, uses the adjusted second set of coefficients during the missile's flight to produce boresight error signals; otherwise, the receiver/processor uses unadjusted first set of error correction coefficients.