Analysis of Ring Laser Gyroscope Cavity Thermal Deformations

Ring laser gyroscopes are crucial for high-precision orientation, stabilization, and autonomous inertial navigation systems. However, their operational accuracy is significantly affected by temperature-induced cavity deformations, leading to potential performance degradation and data loss. This study addresses this challenge by developing a robust algorithm in the MATLAB environment designed to simulate the temperature deformations of a ring laser cavity. Leveraging experimental data, the methodology enables the precise modeling of cavity deformation behavior at various stages of the ring laser gyroscope assembly. The developed mathematical model effectively demonstrates how the addition of structural elements influences the cavity's thermal response and overall deformation. This research provides a novel approach to quantitatively estimate the contribution of individual structural components to the total thermal deformation. The findings offer critical insights for optimizing ring laser gyroscope design, thereby enhancing their accuracy, reliability, and resilience in diverse operational conditions. © 2025 Elsevier B.V., All rights reserved.

Авторы
Sinelnikov
Издательство
International Institute for General Systems Studies
Номер выпуска
1
Язык
English
Страницы
120-131
Статус
Published
Том
2025
Год
2025
Организации
  • 1 RUDN University, Moscow, Russian Federation
Ключевые слова
cavity; control system; inertial measurement unit; inertial navigation systems; mathematical model; MATLAB; ring laser gyroscope; simulation; thermal deformations
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