A kind of metal resonant gyroscope rapid start-up system and method

A metal resonance and gyroscope technology, which is applied in the direction of speed measurement, gyroscope/steering sensing device, speed/acceleration/shock measurement, etc. due to the gyro effect, which can solve the problems of long frequency sweep time, inconvenience, and restriction of gyro engineering. Achieve the effect of improving reliability, wide application range and small signal phase shift

Active Publication Date: 2022-07-26
TIANJIN NAVIGATION INSTR RES INST
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  • Abstract
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Problems solved by technology

However, when the resonant frequency of each resonator has a large difference, it is necessary to expand the frequency sweep range or modify the digital circuit program. If the frequency sweep range is expanded, the frequency sweep time will become longer, resulting in the metal resonator gyroscope not being able to quickly enter a stable working state. The digital circuit program causes a lot of inconvenience to the post-test and other work, which restricts the engineering of the gyroscope.

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  • A kind of metal resonant gyroscope rapid start-up system and method
  • A kind of metal resonant gyroscope rapid start-up system and method

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Embodiment Construction

[0027] The present invention will be further described in detail below through specific examples. The following examples are only descriptive, not restrictive, and cannot limit the protection scope of the present invention.

[0028] A metal resonant gyroscope rapid start-up system, such as figure 1 As shown, it includes a resonator, a buffer circuit, a first low-pass filter module LPF1, a second low-pass filter module LPF2, an analog-to-digital conversion module AD, an FPGA main control chip, a digital-to-analog conversion module DA and a frequency sweep module. The buffer The input end of the circuit is connected to the first output end of the resonator, the first input end of the low-pass filter module is connected to the second output end of the resonator, and the second input end of the low-pass filter module is connected to the output end of the buffer circuit Connected, the input end of the analog-to-digital conversion module AD is connected to the output end of the low-...

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Abstract

The invention relates to a metal resonant gyroscope rapid start-up system and method. Its technical features include: a frequency sweeping module sweeps the frequency of a resonator; an analog-digital conversion module AD collects an excitation signal and an amplitude detection signal generated by the resonator, and then The digital quantity of the excitation signal and the amplitude detection signal is transmitted to the FPGA main control chip; the FPGA main control chip processes the excitation signal and the amplitude detection signal to output a new excitation signal; the digital-to-analog conversion module DA converts the new excitation signal into The analog signal, the analog excitation signal is filtered by a low-pass filter and then applied to the resonator. The invention has a reasonable design, can realize the rapid and stable start-up function of the metal resonant gyroscope under the condition of a wide range of frequency changes, and improves the reliability of the gyroscope.

Description

technical field [0001] The invention belongs to the technical field of inertial instrument control, and relates to a metal resonant gyroscope force feedback working mode, in particular to a metal resonant gyroscope rapid start-up system and method. Background technique [0002] Metal resonant gyroscope is a solid wave gyroscope with simple structure, long life, high reliability and short start-up time. It has broad application prospects in the field of inertial navigation. The core sensitive element of a metal resonant gyroscope is a resonator. Due to factors such as structure, processing, and materials, the resonant frequency of the resonator is usually different. [0003] The resonator is essentially a band-pass filter with frequency selection characteristics. The input signal can pass through the resonator only when the resonant frequency of the resonator is near, and the input signal will have a phase delay of 90° after passing through. When the frequency of the input s...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C19/5691
CPCG01C19/5691
Inventor 王泽涛来琦张悦丛正施贵荣李世杨
Owner TIANJIN NAVIGATION INSTR RES INST
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