Superconducting quantum optical fiber dual-mode fusion inertial navigation system

By fusing superconducting quantum gyroscopes and fiber gyroscopes in inertial navigation systems, and using separators and temperature control modules, the limitations of navigation systems in the prior art in terms of high accuracy and stability are solved, and adapting to various environments is achieved. High-precision navigation effect.

CN119469130APending Publication Date: 2025-02-18POWER (TIANJIN) TECH LTD CO
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Patent Information

Application Number
CN202411720076.1
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-11-28
Publication Date
2025-02-18

AI Technical Summary

Technical Problem

The existing inertial navigation systems have limitations in terms of high accuracy and stability, especially in dynamic environments and harsh weather conditions. The temperature and environmental requirements of superconducting quantum gyroscopes are high, limiting their application range.

Method used

The superconducting quantum fiber dual-mode fusion inertial navigation system is adopted to fuse the superconducting quantum gyroscope and the fiber gyroscope, and use the separator to form two thermally isolated spaces. Combined with the temperature control module, the superconducting quantum gyroscope is ensured in the optimal working state. Run down.

Benefits of technology

It realizes a high-precision and high-stability navigation system, adapts to different environments and weather conditions, expands its application scope, covering fields such as land, aviation, aerospace and navigation.

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Abstract

The invention provides a superconductive quantum optical fiber dual-mode fusion inertial navigation system, and belongs to the field of inertial navigation, the superconductive quantum optical fiber dual-mode fusion inertial navigation system comprises a combined gyroscope and an accelerometer which are fused, the combined gyroscope comprises a shell, a three-axis inertial stabilization platform arranged in the shell, a superconductive quantum gyroscope, an optical fiber gyroscope, a separator, a fusion module and a temperature control module, the superconducting quantum gyroscope and the optical fiber gyroscope are arranged on the three-axis inertially-stabilized platform, the separator is arranged between the shell and the three-axis inertially-stabilized platform to form two thermally-isolated spaces, and the superconducting quantum gyroscope and the optical fiber gyroscope are located in the two spaces respectively. The fusion module is connected with the output end of the superconducting quantum gyroscope and the output end of the optical fiber gyroscope so as to perform fusion processing on two paths of output signals, and the temperature control module and the superconducting quantum gyroscope are located in the same space, so that the superconducting quantum gyroscope operates in the optimal working state. The method is high in precision and stability, is not limited by meteorological conditions, and is wider in application range and higher in adaptability.
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Citation Information

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