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)
Effect of Gyro Noise on ADKEM Gyro-Only Missile System Performance
1991
25 pages
Report
Keine Angabe
Englisch
Missile Guidance & Control Systems , Gyro stabilizers , Noise(Electrical and electromagnetic) , Guided missiles , Kinetic energy , Performance(Engineering) , Degrees of freedom , Hypervelocity weapons , Analog to digital converters , Monte carlo method , Simulation , Gyroscopes , Gyro-only , ADKEM(Advanced Kinetic Energy Missile)
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