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Fully-differential closed-loop fiber-optic gyroscope

A fiber optic gyroscope and full differential technology, applied in Sagnac effect gyroscopes, gyroscopes/steering sensing equipment, measuring devices, etc., can solve problems such as loss, catastrophe, and interference, and achieve simplified use requirements and anti-interference Strong ability to ensure the effect of purity

Pending Publication Date: 2022-02-18
上海傲世控制科技股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The fiber optic gyroscope implemented by the traditional fiber optic gyroscope simulation scheme is extremely vulnerable to external interference in a complex electromagnetic environment. In order to realize its basic functions, a large number of external protection measures have to be taken, which brings great inconvenience to users. , especially in the field of aviation and aerospace, once there is any omission in the external protective measures, the gyroscope is disturbed, as the core sensor of attitude control and inertial navigation, an instantaneous failure will bring catastrophic consequences and cause huge losses

Method used

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  • Fully-differential closed-loop fiber-optic gyroscope
  • Fully-differential closed-loop fiber-optic gyroscope
  • Fully-differential closed-loop fiber-optic gyroscope

Examples

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Embodiment

[0022] Such as figure 1 As shown, a fully differential closed-loop fiber optic gyroscope includes a PIN tube photoelectric signal converter 1, a differential signal amplifier 2, a differential signal sampling type AD3, an FPGA signal processor 4, a differential type D / A output 5, and a differential signal amplifier 6. Y waveguide optical path modulator 7 and gyro sensitive angular velocity full differential output device 8, PIN tube photoelectric signal converter 1, differential signal amplifier 2, differential signal sampling type AD3 are connected with FPGA signal processor 4 in sequence, and the output of FPGA signal processor 4 One path of the signal is transmitted to the gyro-sensitive angular velocity fully differential output device 8 , and the other path is connected to the differential D / A output 5 , the differential signal amplifier 6 and the Y waveguide optical path modulator 7 in sequence.

[0023] The fully differential scheme is used to realize the effect. This s...

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Abstract

The invention relates to a fully-differential closed-loop fiber-optic gyroscope, which comprises a PIN tube photoelectric signal converter, a differential signal amplifier, a differential signal sampling type AD, an FPGA signal processor, a differential type D / A output, a differential signal amplifier, a Y waveguide optical path modulator and a gyroscope sensitive angular velocity fully-differential output device, wherein the PIN tube photoelectric signal converter, the differential signal amplifier and the differential signal sampling AD are sequentially connected with the FPGA signal processor, one path of an output signal of the FPGA signal processor is transmitted to the gyroscope sensitive angular velocity fully-differential output device, and the other path of the output signal of the FPGA signal processor is sequentially connected with the differential D / A output, the differential signal amplifier and the Y waveguide optical path modulator. Compared with the prior art, the effect is realized by adopting a fully differential scheme, and the scheme is high in anti-interference capability, can stably work in various complex electromagnetic environments, simplifies the use requirements of users, and can enable the system to be quickly and stably started in various complex environments to achieve expected functions.

Description

technical field [0001] The invention relates to a fiber optic gyroscope, in particular to a fully differential closed-loop fiber optic gyroscope. Background technique [0002] Gyroscope is a kind of angular rate sensor, which is a device sensitive to angular motion in relative inertial space. It is currently the main sensor used to determine the space motion attitude of moving bodies. Due to cost constraints, it is mainly used in various military fields such as sea, land, air and space. . The fiber optic gyroscope implemented by the traditional fiber optic gyroscope simulation scheme is extremely vulnerable to external interference in a complex electromagnetic environment. In order to realize its basic functions, a large number of external protection measures have to be taken, which brings great inconvenience to users. , especially in the field of aviation and aerospace, once there is any omission in the external protective measures and the gyroscope is disturbed, as the co...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C19/72
CPCG01C19/721
Inventor 吴海林白亮虞翔李阳杨涛施广飞俞岭
Owner 上海傲世控制科技股份有限公司
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