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Digital closed-loop optical fiber gyroscope full-loop detection and simulation test system

A fiber optic gyroscope and simulation test technology, applied in the field of inertial attitude sensor system, can solve the problem of inability to test the bandwidth of fiber optic gyroscope, and achieve the effect of avoiding self-limitation

Active Publication Date: 2014-06-25
BEIJING INST OF CONTROL ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Limited by the conditions of the mechanical equipment such as the sudden stop table and the angular vibration table, it is impossible to do a limit test on the bandwidth of the fiber optic gyroscope.

Method used

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  • Digital closed-loop optical fiber gyroscope full-loop detection and simulation test system

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Embodiment Construction

[0031] In the digital closed-loop fiber optic gyroscope, the external angular velocity is used as the input signal to cause the phase difference between the forward and reverse beams. As a feedback signal, the step wave is added to the phase modulator, which also causes a phase difference between the two beams of light. The phase difference is proportional to the step height of the step wave and is given by the digital signal processing circuit. Using a specific step wave (sine, or step) to simulate the required external angular velocity input signal can easily realize the optical path of the fiber optic gyroscope, the function detection of the circuit, the test of the dynamic characteristics and the realization of the dynamic simulation function.

[0032] In the digital closed-loop fiber optic gyroscope, both the feedback signal and the output signal are the step height of the digital staircase wave calculated by the digital controller. The principle block diagram of the digi...

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Abstract

The invention discloses a digital closed-loop optical fiber gyroscope full-loop detection and simulation test system which comprises an optical system module, a pre-amplification module, a digital processing module, a feedback module, a communication module and a ground detection and simulation test system. Under a condition of no turntable, the digital closed-loop optical fiber gyroscope full-loop detection and simulation test system can realize full-loop detection on an optical fiber gyroscope; under a condition of no angle vibration table and sudden stop table, a stand-alone bandwidth test on the optical fiber gyroscope can be implemented; the self-condition limitation of the conventional mechanical equipment is avoided in a test process; under a condition that any auxiliary ground detection circuit is not added, a dynamic simulation function of a branch system can be realized, and parameter limitation caused by auxiliary circuits is avoided; complicated dynamic simulation is implemented. According to the digital closed-loop optical fiber gyroscope full-loop detection and simulation test system, the power consumption and weight of a product are reduced, and the cost is lowered; minimized and low-cost design of the product is realized.

Description

technical field [0001] The invention belongs to the technical field of inertial attitude sensor systems, and relates to a digital closed-loop fiber optic gyroscope full-loop detection and simulation test system. Background technique [0002] In recent years, due to the prosperity of the micro-satellite market, the research on low-cost and miniaturized inertial attitude sensors has developed rapidly. In order to perform ground physical simulation for satellite products, all stand-alone machines must have a ground detection function, so it is necessary to increase the auxiliary circuit to realize the ground detection function, which increases the power consumption, size and weight of the product. [0003] As an important frequency characteristic, bandwidth test is an important content of gyroscope performance test. The traditional method is to use mechanical equipment such as sudden stop table and angular vibration table to obtain the frequency response curve, and then calcul...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C25/00
CPCG01C25/00
Inventor 张金保林松孙丽高晨光付明睿王冲李勇马官营赵亚飞
Owner BEIJING INST OF CONTROL ENG
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