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Z-axis gyroscope neural network sliding mode control method based on disturbance observer

A technology of disturbance observer and neural network, applied in gyroscope/steering sensing equipment, adaptive control, general control system, etc., can solve problems such as upper bound of disturbance, strong chattering, etc., to improve measurement accuracy and compensate system parameters Errors and external disturbances, the effect of improving the control effect and parameter estimation effect

Active Publication Date: 2020-04-17
NANTONG UNIVERSITY
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AI Technical Summary

Problems solved by technology

However, in practical situations, the upper bound of external interference is unknown
At this time, a larger switching gain needs to be selected, which will cause stronger chattering

Method used

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  • Z-axis gyroscope neural network sliding mode control method based on disturbance observer
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  • Z-axis gyroscope neural network sliding mode control method based on disturbance observer

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Embodiment Construction

[0047] In order to further understand the present invention, the preferred embodiments of the present invention are described below in conjunction with the examples, but it should be understood that these descriptions are only to further illustrate the features and advantages of the present invention, rather than limiting the claims of the present invention.

[0048] Please refer to figure 1 , the present invention provides a Z-axis gyroscope neural network sliding mode control method based on disturbance observer, comprising the following steps:

[0049] 1) Establish a micro-gyroscope dynamics model, output the micro-gyroscope motion track according to the model:

[0050] The mathematical model of the micro gyroscope is:

[0051]

[0052] Among them, x and y are the displacement of the micro gyroscope in the direction of X and Y axes, u x , u y is the control input of the micro gyroscope in the direction of X and Y axes, d xx 、d yy is the elastic coefficient of the spri...

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Abstract

The invention discloses a Z-axis gyroscope neural network sliding mode control method based on a disturbance observer. According to the method, an RBF neural network is adopted to estimate a time-varying angular velocity parameter matrix on the basis of obtaining a micro-gyroscope tracking error and a designed sliding mode surface, an interference observer is designed to estimate external interference under the condition that the external interference is unknown, and a micro-gyroscope control law is designed according to the estimated time-varying angular velocity parameter matrix and the interference observer. Finally, a continuously changing angular velocity signal and unknown external interference are estimated correctly. According to the method, the neural network can be adopted to estimate the time-varying angular velocity under the condition that the angular velocity is continuously changed, and the adaptive adjustment of the weight is completed by designing the neural network weight adaptive rule. Meanwhile, under the condition that the external interference of the system is unknown, the interference observer is adopted to estimate the external interference, so that the buffeting of the system is effectively reduced, and the measurement precision of the MEMS gyroscope is improved.

Description

technical field [0001] The invention relates to the field of automatic control systems, in particular to a Z-axis gyroscope neural network sliding mode control method based on disturbance observers. Background technique [0002] MEMS gyroscope is a sensor produced by micro-electromechanical system processing technology, which is used to measure angular velocity. MEMS gyroscopes can be divided into vibration type, microfluidic type, solid type and suspended rotor type. The most common of these is the vibrating MEMS gyroscope. The MEMS gyroscope uses the Coriolis theorem to convert the angular velocity of a rotating object into a DC voltage signal proportional to the angular velocity, thereby calculating the angular velocity. MEMS gyroscopes have the advantages of small size, low power consumption, and low cost, and have broad application prospects in inertial navigation, consumer electronics, and modern defense. Due to defects in manufacturing technology, the structure of ...

Claims

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Application Information

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IPC IPC(8): G05B13/04G01C19/5776G01C25/00
CPCG05B13/042G01C19/5776G01C25/00
Inventor 卢成王慧敏付建源朱宁远张小虎
Owner NANTONG UNIVERSITY
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