scholarly journals Precision Angle Measurement Systems on the Basis of Ring Laser Gyro

Sensors ◽  
2020 ◽  
Vol 20 (23) ◽  
pp. 6930
Author(s):  
Yuri V. Filatov ◽  
Petr A. Pavlov ◽  
Alexander A. Velikoseltsev ◽  
K. Ulrich Schreiber

The main application of a ring laser gyroscope is navigation. It is currently the most widely used device for strapdown inertial navigation systems. However, it is also applicable for high-precision angle metrology systems. This paper discusses the properties of a laser dynamic goniometer (LDG) based on the ring laser gyroscope and designed for the calibration of optical polygons and digital angle converters, and for the measurement of angles between external mirrors (theodolite operating mode). We consider the main sources of uncertainty, such as the ring laser gyro bias due to an external magnetic field and the instability caused by the velocity of rotation along with applicable methods of their compensation. The reversal method providing separation of uncertainties of the LDG and the calibrated angle converter is analyzed in detail. The simplified cross-calibration method is also considered. The results of calibration of optical encoders of various designs—with and without their own rotors (on-axis and off-axis in Euramet terminology)—are presented. Some results of the dynamic goniometer for the measurement of angles between external mirrors are presented. It is shown that the LDG in this mode of operation demonstrates better accuracy than modern theodolites and total stations.

2013 ◽  
Vol 2013 ◽  
pp. 1-7 ◽  
Author(s):  
Jianli Li ◽  
Yanhai Ma ◽  
Chen Xiyuan

In order to improve the precision of Strapdown Inertial Navigation System (SINS) and reduce the complexity of the traditional calibration method, a novel calibration and compensation scheme is proposed. An optimization calibration method with four-direction rotations is designed to calculate all error coefficients of Ring Laser Gyroscope (RLG) SINS in a series of constant temperatures. According to the actual working environment, the temperature errors of RLG SINS are compensated by a nonlinear interpolation compensation algorithm. The experimental results show that the inertial navigation errors of the proposed method are reduced.


2009 ◽  
Vol 1 (1) ◽  
pp. 564-567 ◽  
Author(s):  
T. Hashimoto ◽  
J. Maeya ◽  
T. Fujita ◽  
K. Maenaka

1993 ◽  
Vol 47 (1) ◽  
pp. 543-551 ◽  
Author(s):  
Fabien Bretenaker ◽  
Bruno Lépine ◽  
Annie Le Calvez ◽  
Olivier Adam ◽  
Jean-Paul Taché ◽  
...  

2005 ◽  
Vol 119 (1) ◽  
pp. 75-83 ◽  
Author(s):  
Wang Kedong ◽  
Yan Lei ◽  
Gu Qitai

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