LCR- 100罗经ahrs系统是寻北姿态航向参考系统，基于最先进的光纤陀螺和微机电(MEMS)加速度计。
The LCR-100 Gyrocompass AHRS is a north finding attitude and heading reference system based on a state-of-the-art fibre-optic gyro and micro-electromechanical (MEMS) accelerometers.
通常放置在标准惯性参考系统中，陀螺仪能够使设备在瞬间建立精确的航向，而不使用磁通阀或者磁力计。
Normally found in standard inertial reference systems, gyro-compassing enables the unit to establish precise heading within moments, without the use of a magnetic flux valve or magnetometer.
由仿真结果可以看出，它能较精确地估计陀螺常值漂移和航向角误差，为系统误差的校正提供了可信信息。
The simulation results show that the constant gyro drifts and the heading errors, which provide information for calibrating the system errors, can be estimated exactly.
战车用惯性定位定向系统由于采用双轴陀螺平台结构，不可避免地存在着支架误差，从而影响系统航向精度。
The inertial system of fighting vehicle existed bracket error due to its two-axis gyro platform structure, and this could influence the heading precision.
研制了一种由数字磁罗盘和角速度陀螺组成的组合航向系统。
A combined heading system including a digital magnetic compass and a rate gyroscope is developed.
因此，单独使用陀螺仪也无法保持飞机的特定航向。
So, gyros alone can't be used to keep in an aircraft in a particular orientation.
经常核对陀螺罗经和磁罗经航向。
摘要：研究了基于硅mems陀螺、加速度计及磁阻式磁强计组合的微小型飞行器用姿态航向参考系统。
Abstract: an integrated micro attitude heading reference system (MAHRS) was researched for micro aerial vehicles (MAV) based on the MEMS gyroscopes, accelerometers, and magnetic-sensors.
研究了基于硅mems陀螺、加速度计及磁阻式磁强计组合的微小型飞行器用姿态航向参考系统。
An integrated micro attitude heading reference system (MAHRS) was researched for micro aerial vehicles (MAV) based on the MEMS gyroscopes, accelerometers, and magnetic-sensors.
文章介绍了陀螺罗经航向信号数字化处理系统的软、硬件结构，数字航向的显示，罗经性能参数的测试方法。
This paper introduces the software and hardware structure, display of digital course and the testing method of compass parameter of gyrocompass course signal digital processing system.
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).
研究一种应用于船舶的GPS/单陀螺航向融合算法。
This paper introduces a GPS/single gyro yaw value fusion algorithm for marine application.
这个航向可以纠正偏航陀螺的漂移，从而实现航向锁定。
This heading can correct the gyro yaw drift to achieve heading lock.
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.
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