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Force feedback control system and method for hemispherical resonator gyroscope

A hemispherical resonant gyroscope and control system technology, used in gyroscope/steering sensing equipment, gyro effect for speed measurement, instruments, etc., and can solve problems such as poor external temperature adaptability

Active Publication Date: 2017-03-08
BEIJING INST OF CONTROL ENG
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  • Application Information

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Problems solved by technology

[0004] Problems solved by the technology of the present invention: overcome the problem of poor adaptability of the existing analog force feedback control loop to the external temperature, and provide a force feedback control method that can adapt to the influence of the temperature change of the external environment of the hemispherical resonant gyroscope on the hemispherical resonant gyroscope , especially a force feedback control system and control method for a hemispherical resonant gyroscope, the method and system can ensure the control accuracy of the force feedback control loop and the stability of the performance of the hemispherical resonant gyroscope

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  • Force feedback control system and method for hemispherical resonator gyroscope
  • Force feedback control system and method for hemispherical resonator gyroscope
  • Force feedback control system and method for hemispherical resonator gyroscope

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Embodiment

[0076] A force feedback control system for a hemispherical resonant gyroscope, the control system includes a weak signal detection module 100, a signal preprocessing module 200, a node signal amplitude demodulation module 300, a frequency synchronization tracking module 400, a controller 500, and a feedback signal modulation Module 600 and drive signal high-voltage conversion module 700;

[0077] Such as Figure 9 As shown, the weak signal detection module 100 outputs a signal V1 and an output signal V2;

[0078] The signal preprocessing module 200 outputs a signal V3;

[0079] The node signal amplitude demodulation module 300 outputs signal V4;

[0080] The controller 500 outputs a signal V5;

[0081] The frequency synchronization tracking module 400 outputs an AC signal V6;

[0082] The feedback signal modulation module 600 outputs a signal V7;

[0083] Such as Figure 10 As shown, the signals between the internal modules of the frequency synchronization tracking modul...

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Abstract

The invention relates to a force feedback control system and method for a hemispherical resonator gyroscope and belongs to the technical field of control of inertial instruments; the control system and method are applied to a force feedback working mode of the hemispherical resonator gyroscope, and the method is a way to implement a hemispherical resonator gyroscope control method. By using a hemispherical resonator gyroscope force feedback circuit designed by using the method, it is possible to synchronously track the operating frequency of the hemispherical resonator gyroscope, demodulate the amplitude and phase of gyroscope wave node signals, and modulate high-voltage signals of force feedback control signals; in addition, not by modifying the configuration of a controller but just correcting controller parameters, it is possible to meet different environmental application needs of the hemispherical resonator gyroscope.

Description

technical field [0001] The invention relates to a force feedback control system and control method of a hemispherical resonant gyroscope, belonging to the technical field of inertial instrument control. The control system and control method are applied in the force feedback working mode of the hemispherical resonant gyroscope, and are a control method of the hemispherical resonant gyroscope A way of realizing . Background technique [0002] The inertial instrument is one of the important components in the aerospace vehicle control system, which is used to measure the attitude information of the aerospace vehicle. The hemispherical resonant gyroscope is a new type of solid-state vibrating gyroscope with long life, high reliability and radiation resistance. It is one of the important choices of inertial measurement components in aerospace vehicle control systems. The United States took the lead in the development of hemispherical resonant gyroscopes in the 1960s, and countrie...

Claims

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Application Information

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IPC IPC(8): G01C19/5776
CPCG01C19/5776
Inventor 李建朋武志忠冯士伟刘吉利李恺付明睿王月李杰彦
Owner BEIJING INST OF CONTROL ENG
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