Suppression of the G-sensitive drift of laser gyro in dual-axis rotational inertial navigation system

• 作者: YU Xudong WANG Zichao FAN Huiying WEI Guo WANG Lin
• 来源期刊: 系统工程与电子技术（英文版）
• 年，卷（期）: 2021,（4）
• 所属期刊栏目: ELECTRONICS TECHNOLOGY
• 页码范围: 822-830
• 页数: 9页
• 语种: 英文
• DOI: 10.23919/JSEE.2021.000071

摘要

The dual-axis rotational inertial navigation system (INS) with dithered ring laser gyro (DRLG) is widely used in high precision navigation. The major inertial sensor errors such as drift errors of gyro and accelerometer can be averaged out, but the G-sensitive drifts of laser gyro cannot be averaged out by in-dexing. A 16-position rotational simulation experiment proves the G-sensitive drift will affect the long-term navigation error for the rotational INS quantitatively. The vibration coupling and asymmetric structure of the DRLG are the main errors. A new dithered mechanism and optimized DRLG is designed. The validity and efficiency of the optimized design are conformed by 1 g sinusoidal vibration experiments. An optimized inertial measu-rement unit (IMU) is formulated and measured experimentally. Laboratory and vehicle experimental results show that the diver-gence speed of longitude errors can be effectively slowed down in the optimized IMU. In long term independent navigation, the position accuracy of dual-axis rotational INS is improved close to 50％, and the G-sensitive drifts of laser gyro in the optimized IMU are less than 0.0002 °/h. These results have important theo-retical significance and practical value for improving the structu-ral dynamic characteristics of DRLG INS, especially the high-precision inertial system.