Effect of Gyro Noise on ADKEM Gyro-Only Missile System Performance.

摘要

This report presents results from a series of deterministic and Monte Carlo runs which indicate that the addition of three bits of noise to the sixteen bit A/D converter used with the gyros that will be mounted on the gyro-only demonstration ADKEM flight vehicles will not adversely affect system performance. These results are based on modeling the three bits of noise on the gyros and using Monte Carlo statistical analysis to quantify its effects on system performance. (Author)