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Simulation method for digital closed-loop control logic of fiber-optic gyroscope

A technology of fiber optic gyroscope and simulation method, which is applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve the problems of wasting resources, repeated design, etc., and achieve the effect of improving work efficiency, reducing product cost, and shortening project cycle

Active Publication Date: 2014-08-13
HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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Problems solved by technology

[0003] Aiming at the above defects or improvement needs of the prior art, the present invention provides a simulation method for the digital closed-loop control logic of the fiber optic gyroscope. A large number of codes are used to realize the digital closed-loop control of the fiber optic gyroscope. If there is a problem, it can only be exposed in the debugging stage, resulting in repeated design and technical problems that waste resources.

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[0030] 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. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0031] The simulation method of the fiber optic gyroscope digital closed-loop control logic provided by the present invention adopts a top-down design idea, first performs system-level modeling and simulation, and then automatically converts the model into a hardware description language code through System Generator software. This method frees designers from writing detailed codes and puts more...

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Abstract

The invention provides a simulation method for the digital closed-loop control logic of a fiber-optic gyroscope. The simulation method comprises the following steps: establishing a model and simulating according to the model, wherein a fiber-optic gyroscope closed-loop control logic model comprises a digital demodulation model and a digital controller model, and a closed-loop control logic simulation fiber-optic gyroscope model comprises a Sagnac effect model, a deviation modulation model, a step modulation model and phase modulation model; determining parameters needed by simulation, wherein the parameters comprise a system loop closing cycle, a modulation square wave frequency f, a square wave half-cycle sampling point number and a magnification factor; adjusting the magnification factor of a pre-amplifier module and the magnification factor of a post-amplifier module to realize normal loop closing of the fiber-optic gyroscope model in a simulation process; determining whether the output scale factor of the fiber-optic gyroscope is consistent with a required index or not through the waveform and numerical value of an output signal. By adopting the simulation method, designers do not need to perform detailed coding writing and can put more effort into system design and analysis; the project period can be shortened, the working efficiency is increased, and the product cost is reduced.

Description

technical field [0001] The invention belongs to the field of inertial device fiber optic gyroscopes, and more specifically relates to a simulation method for digital closed-loop control logic of fiber optic gyroscopes. Background technique [0002] At present, the logic design method of digital closed-loop fiber optic gyroscope is completed by first writing code, simulating, and then synthesizing the code, layout and wiring. Designing gyro logic in this way requires designers to be familiar with the hardware description languages ​​VHDL and Verilog HDL, and manually write a large amount of code, and then convert the code into specific hardware logic for implementation. At the same time, due to the separate design of the closed-loop control logic, which is separated from the environment of the gyro closed-loop system, it is impossible to simulate and analyze design issues such as logic and digital control from the perspective of the entire system. The problems need to be expo...

Claims

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Application Information

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IPC IPC(8): G06F17/50
Inventor 黎秋甫王爱民焦守江李永江
Owner HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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