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

Abstract

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)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1991
Accession Number
ADA246150

Entities

People

  • Vicki C. Lefevre

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Human Systems
  • Weapons Technologies

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  • Aerodynamics/Aeronautics.
  • Computational Modeling and Simulation
  • Radio communications and signal processing.