该电路也是在制导控制系统和导航系统的高性能陀螺仪的使用。
This circuitry is also in use in high-performance gyroscopes in guidance control systems and navigation systems.
实验仿真结果表明，与无陀螺捷联惯导系统相比，该组合导航系统的精度和容错性能显著提高。
Computer simulation results show that, the precision and fault tolerance of the integrated navigation system are improved greatly, compared with the pure GFSINS.
如果陀螺仪发生故障，天体导航系统就会接替它继续进行工作。
Should the gyroscopes break down, the celestial system would take over.
当惯性陀螺工作在方位姿态时，有一定的斜坡漂移，它将引起惯性导航系统中的严重的航向和位置误差，所以有必要估计和补偿它。
There exists a slope drift in an integral gyro when it is used as an azimuth gyro, which may cause serious heading and position errors in the Inertial Navigation System (INS).
详细描述了捷联惯性导航系统（SINS）中加速度计和陀螺数据仿真的方法，并给出了求解扰动重力的算法。
The simulative methods about the data of accelerator and gyro embedded in SINS are described in detail, and the algorithm about the disturbing gravity is presented.
提高角速度解算精度是提高无陀螺惯性导航系统导航参数解算精度的主要途径。
Improving the accuracy of angular resolution is the key way to improve the navigation parameter resolution precision of accelerometer based gyro-free inertial navigation system.
介绍了船用捷联惯性导航系统中陀螺仪数据采集系统的设计。
The design of gyroscope data acquisition system for Marine strapdown inertial navigation system is presented.
本文应用天文导航理论，根据GPS提供的位置信息，对静电陀螺捷联导航系统陀螺常值漂移和载体航向角进行校正的算法进行了研究。
Using astronavigation theory, the algorithm of calibrating the constant gyro drifts of ESG strapdown inertial navigation system and carrier heading is presented in this paper.
本文以实际工程项目为背景—船用平台式惯性导航系统，对陀螺仪的各种漂移的建模及补偿进行了研究。
This dissertation, based on the development task background of a project - gimbaled Inertial Navigation System for Ship, addresses the modeling and compensation of gyros drifts in a gimbaled INS.
捷连惯性导航系统SINS- 500是基于TRS - 500的光纤陀螺仪、精密加速度传感器以及板式集散地。
Strapdown Inertial Navigation System SINS-500 is based on Optolink's TRS-500 FOGs, precise accelerometers and board computer.
捷连惯性导航系统SINS- 1000是基于SRS - 1000的光纤陀螺仪、精密加速度传感器以及板式集散地。
Strapdown Inertial Navigation System SINS-1000 is based on Optolink's SRS-1000 FOGs, precise accelerometers and board computer.
随着陀螺精度的不断提高，在惯性导航系统中对高精度加速度计的需求越来越迫切。
As the precision improvement of gyroscope, the requirement of high precision accelerometer was much imminence in inertial field.
该陀螺仪性能好、体积小、功耗低，在中等精度的惯性导航系统中有较好的应用前景。
The proposed vibratory gyroscope has a promising prospect for the inertial navigation system with a medium accuracy due to its high performance, small volume and low power consumption.
本文从惯性导航基本方程出发，推导了激光陀螺捷联式惯性导航系统的系统级标定的一种误差标定模型。
In this paper, based on the inertial navigation equation, a novel model for the laser gyro strapdown inertial navigation system is provided.
本文从惯性导航基本方程出发，推导了激光陀螺捷联式惯性导航系统的系统级标定的一种误差标定模型。
In this paper, based on the inertial navigation equation, a novel model for the laser gyro strapdown inertial navigation system is provided.
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