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Method, device, system and medium for identifying error of rate-integrating gyroscope detection electrode

A detection electrode and identification method technology, applied in the field of rate integration gyro detection electrode error identification, can solve problems such as the impact of rate integration gyro performance, gyro detection electrode error, control loop detection gain, etc., to achieve rapid identification of detection electrode error compensation parameters, High precision and intuitive effect of error parameter identification

Active Publication Date: 2021-11-09
NAT UNIV OF DEFENSE TECH
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Problems solved by technology

However, due to the influence of processing and assembly errors, gyroscopes usually have detection electrode errors, resulting in detection gain and angle errors in the control loop, which have a greater impact on the performance of rate-integrating gyroscopes

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  • Method, device, system and medium for identifying error of rate-integrating gyroscope detection electrode
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  • Method, device, system and medium for identifying error of rate-integrating gyroscope detection electrode

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Embodiment Construction

[0057] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0058] The method for identifying the error of the detection electrode of the rate-integrating gyroscope provided in an embodiment of the present invention includes the following steps:

[0059] S1. Collect the measured output data of the rate-integrating gyroscope with detection electrode errors under high-speed rotation, and obtain the angle estimation error of the mode shape angle;

[0060] S2. Perform component analysis based on the angle estimation error to obtain the in-phase component and quadrature component of the angle estimation error;

[0061] S3. Calculate the magnitude of the angle e...

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Abstract

A method, device, system, and medium for identifying an error in a rate-integrating gyro detection electrode, comprising: collecting actual output data of a rate-integrating gyroscope with a detection electrode error under high-speed rotation, and obtaining an angle estimation error of a mode shape angle; Composition analysis to obtain the in-phase component and quadrature component of the angle estimation error; judge whether the detection electrode error parameter identification has reached the expected accuracy based on the magnitude of the angle estimation error; value and the amplitude of the quadrature component, adjust the detection electrode error compensation parameter, and compensate the detection electrode error in the measured output data until the detection electrode error parameter identification reaches the expected accuracy, and output the corresponding detection electrode error compensation parameter. The invention has the characteristics of high speed, high precision and high degree of automation, and is suitable for the batch debugging process of the rate integrating gyroscope.

Description

technical field [0001] The invention relates to the technical field of solid-state vibrating gyroscopes, in particular to a method, device, system and medium for identifying errors in detection electrodes of rate-integrating gyroscopes. Background technique [0002] The gyroscope is a sensor that detects the angular motion of the carrier. It plays a key role in the fields of inertial navigation and attitude control. Its performance directly determines the accuracy of the inertial navigation and attitude control system. [0003] The current gyroscopes include: mechanical rotor gyroscopes, solid-state vibration gyroscopes and optical gyroscopes. Compared with mechanical rotor gyroscopes, solid-state vibration gyroscopes have simple structures and no rotating parts, so they have outstanding advantages such as high reliability, good impact resistance, small size, and low cost. Compared with optical gyroscopes, solid-state vibrating gyroscopes only need a single resonant structu...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C25/00
CPCG01C25/005
Inventor 张勇猛孙江坤余升肖定邦吴学忠吴宇列席翔李青松卢坤石岩周鑫
Owner NAT UNIV OF DEFENSE TECH
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