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Reliability analysis process and reliability improvement of an inertial measurement unit (IMU)
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Date
2010
Author
Ünlüsoy, Özlem
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Reliability is one of the most critical performance measures of guided missile systems. It is directly related to missile mission success. In order to have a high reliability value, reliability analysis should be carried out at all phases of the system design. Carrying out reliability analysis at all the phases of system design helps the designer to make reliability related design decisions in time and update the system design. In this study, reliability analysis process performed during the conceptual design phase of a Medium Range Anti-Tank Missile System Inertial Measurement Unit (IMU) was introduced. From the reliability requirement desired for the system, an expected IMU reliability value was derived by using reliability allocation methods. Then, reliability prediction for the IMU was calculated by using Relex Software. After that, allocated and predicted reliability values of the IMU were compared. It was seen that the predicted reliability value of the IMU did not meet the required reliability value. Therefore, reliability improvement analysis was carried out.
Subject Keywords
Rockets.
URI
http://etd.lib.metu.edu.tr/upload/12612387/index.pdf
https://hdl.handle.net/11511/19954
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Graduate School of Natural and Applied Sciences, Thesis
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Ö. Ünlüsoy, “Reliability analysis process and reliability improvement of an inertial measurement unit (IMU),” M.S. - Master of Science, Middle East Technical University, 2010.