Fiber-optic gyroscope assembly with separated optically sensitive part and signal processing part

A technology of sensitive components and signal processing, applied in the field of inertial measurement, can solve problems such as increased weight, disadvantageous lightweight design, etc., to achieve the effects of weight reduction, convenient redundant design, and low power consumption

Active Publication Date: 2017-11-17
BEIJING AEROSPACE TIMES OPTICAL ELECTRONICS TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] In the existing fiber optic gyroscope assembly, the integrated design is generally adopted, and the optical sensitive components and signal processing components are installed on a structure. This design method is widely used in low-precision products and can be used in small Angular velocity measurement can be achieved with a small volume and light weight, but for very high-precision products, due to the large volume of the instrument, in order to ensure the mechanical properties, it is necessary to increase the thickness of the structure to ensure the adaptability to the mechanical environment, which increases the product. Weight, not conducive to lightweight design

Method used

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  • Fiber-optic gyroscope assembly with separated optically sensitive part and signal processing part
  • Fiber-optic gyroscope assembly with separated optically sensitive part and signal processing part
  • Fiber-optic gyroscope assembly with separated optically sensitive part and signal processing part

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Embodiment

[0038] In this embodiment, the fiber optic gyroscope assembly includes two parts, an optical sensitive component and a signal processing component. The optical sensitive component includes three fiber optic gyroscopes and a structural body, and the signal processing component includes three signal processing circuits and a secondary power supply. Modules and structural parts, wherein the secondary power supply module includes three secondary power supply circuits, such as figure 1 shown.

[0039] Each secondary power supply circuit supplies power to a fiber optic gyroscope and a signal processing circuit respectively. A magnetic latching relay is set in the secondary power supply circuit. The magnetic latching relay receives the on-off control command of the attitude control system, and the on-off control The command controls the magnetic latching relay to open and close to realize the on-off control of the power supply circuit; the on-off command is an open collector output, th...

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Abstract

The invention discloses a fiber-optic gyroscope assembly with separated optically sensitive part and signal processing part. The optically sensitive part comprises three totally independent fiber-optic gyroscopes. The sensitive axes of the gyroscopes are orthogonally and obliquely arranged on the lateral surface of a cone with a semi-cone angle of 54 degree 44' 08''. The signal processing part comprises three totally independent signal processing circuits and one secondary power supply module. The secondary power supply module comprises three totally independent secondary power supply circuits. For electrical functions, the assembly comprises three totally independent angular velocity measuring channels; each channel comprises one secondary power supply circuit, one signal processing circuit, and one fiber-optic gyroscope; the independence of measurement is improved; at the same time, the fault isolation is realized, the reliability of the assembly is enhanced; a three axes oblique arrangement scheme is adopted so that the assembly can conveniently cooperate with other gyroscope assemblies to carry out redundancy configuration, and the measurement precision is improved.

Description

technical field [0001] The invention relates to the technical field of inertial measurement, in particular to an optical fiber gyroscope assembly in which an optical sensitive component and a signal processing component are separated. Background technique [0002] Fiber optic gyroscope is a new type of inertial instrument based on the Sagnac effect. It has the advantages of small size, light weight, low power consumption, high reliability and long life. It has unique advantages in the field of space inertial technology and is widely used in space vehicles. in the guidance, navigation and control system. [0003] In the existing fiber optic gyroscope assembly, an integrated design is generally adopted, and the optical sensitive components and signal processing components are installed on one structure. This design method is widely used in low-precision products and can be used in smaller The angular velocity measurement can be realized under the small volume and light weight...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C19/64G01C19/72
CPCG01C19/64G01C19/728
Inventor 孟祥涛向政古俊豪杨永斌李超谢海峰杨克成苏立娟
Owner BEIJING AEROSPACE TIMES OPTICAL ELECTRONICS TECH
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