Practical simulating models are deduced and built for the gyro system and the performing setting of the servo system to consist a close-control loop with angle-tracing circuit.
推导并建立了陀螺系统和伺服执行机构的实物仿真模型，使之与角跟踪电路构成闭合控制回路。
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.
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 state equations of the system are established on the basis of the relation between attitude error quaternion and the gyro drift.
本文以姿态误差四元数与陀螺漂移误差之间的关系为基础，构建了系统状态方程；
A system of measurement and analysis is developed to improve the accuracy and efficiency of measurement and to control the dynamic performance of gyro motor.
为了提高陀螺电机动态性能的测试精度和测试效率，进而控制该性能，开发了一套测试、分析系统。
This paper introduces the traditional control method of Gyro temperature control system, and gives the digital PID control method of the gyro temperature control based on PC/104.
介绍了陀螺温控系统的传统控制方法，并在此基础上提出了基于PC/104的数字PID控制的陀螺温度控制方法。
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.
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。
In the resonator fiber-optic gyro (R-FOG), the detection precision of the system is influenced by the polarization-fluctuation deeply.
谐振式光纤陀螺(R - FOG)中，偏振波动引起的检测信号漂移对陀螺系统的检测精度有重要影响。
As the demanding for high accuracy Ring Laser Gyro is increasing in our country, FPGA is implemented in the control system of the RLG.
针对国内对高精度环形激光陀螺(RLG)的需求，本文把FPGA应用于激光陀螺控制系统之中。
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).
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。
Action parameters are quickly stored in the testing system, and the problem that the projectile-borne mechanism is influenced by the surroundings in the gyro simulation test is solved.
该测试系统能直接将动作参数高速存储，并较好地解决陀螺模拟试验装置中弹载机构受外界环境影响较大的问题。
At last, the hardware in the loop simulation system for three-axis stabilized satellite attitude control based on PC, with reaction wheel and gyro in the loop is designed.
最后，该文设计了一个基于PC机的三轴稳定卫星姿态控制硬件在回路仿真系统，将反作用飞轮、陀螺等实物接入仿真系统。
To get high accuracy of satellite attitude determination, a new approach of satellite attitude determination system, which combines the star-sensors with gyro, is presented in the article.
为了满足军用卫星姿态测量高精度的需要，提出了基于状态估计法的陀螺仪和星敏感器组成的卫星姿态测量系统的方案。
This paper presents the design and actual circuit of a computer control system for the North-Seeker with ARM7 (here LPC2292 is used) as core microprocessor and the flexible gyro as sensor.
介绍了一种以arm7单片机(选用LPC 2292)作为核心处理器，以挠性陀螺为传感器的寻北仪方位角-数字转换系统设计及实现电路。
The article also studied the tracking quality in which the system has used the motor encoder and the velocity gyro as the velocity loop feedback respectively.
研究了分别以电机编码器和速率陀螺输出信号作为速度环反馈时，系统输出的跟踪特性。
The laser gyro inertial surveying and attitude reference system model with incomplete inertial sensors are first derived under the body dynamic constraint.
首次推导了非完整惯性传感器配置条件下，基于载体动态约束的激光陀螺惯性测量与姿态参考模型。
The detection theory of resonator fiber optic gyro (R-FOG) based on the serrodyne modulation with two frequencies was introduced, and the correlative detection theory in digital system was analyzed.
介绍了基于双频率锯齿波组合调制的谐振式光纤陀螺(R - FOG)的检测原理，分析了数字系统信号相关检测的理论。
The experiment result can approve that the gyro has a preferable precision, the dither bias system work perfectly and the target of dither bias is achieved.
测试结果表明：所研制的机械抖动激光陀螺具有较高的精度，抖动偏频系统工作稳定，抖动偏频消闭锁的目标得到了较好的实现。
The micro gyro three-dimensional track and localization includes four stages, such as triggering system, acquiring data, enlarging and changing signal, storing and keeping data.
微陀螺三维跟踪定位，通过系统触发、采集数据、放大转换和存储保持四个阶段完成。
A larger high-frequency noise in the output signal of fiber optic gyro lowers the calculation accuracy of fiber optic gyro attitude system.
光纤陀螺输出信号中存在较大的高频噪声，这降低了光纤陀螺姿态系统的解算精度。
The inertial system of fighting vehicle existed bracket error due to its two-axis gyro platform structure, and this could influence the heading precision.
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 software system of gyro drift testing is introduced and it is carried out by VB finally.
最后介绍了利用VB语言设计陀螺漂移测试的软件系统。
In this paper, a one-step ahead predictive control algorithm based on wavelet neural networks is proposed for the gyro stability tracking system with high accuracy.
针对高精度陀螺稳定跟踪系统，提出了一种基于小波基函数神经网络的非线性系统的一步超前预测控制算法。
Single gyro strapdown inertial navigation system (SGSINS) has many advantages, for example, small volume, light weight, low cost, high reliability and so on.
单陀螺捷联惯导系统（SGSINS）不仅具有和经典捷联惯导系统相同的基本功能，而且有体积小、重量轻、成本低、可靠性高等优点。
Thereupon, the gyro dynamic characteristics have been greatly improved and the performance of the wide frequency band system have been met.
从而可以大幅度提高陀螺的动态性能，满足宽频带系统的性能要求。
In this paper an on-line automatic testing system is introduced which detects the output and loop state variables of a pendulous integrating gyro accelerometer (PIGA) by means of computers.
本文介绍一种针对摆式积分陀螺加速度计(PIGA)的输出与回路状态变量进行实时测试的自动化测试系统。
At the same time, the accumulated error of traverse measurement is effectively controlled by use of a gyro orientation system.
同时采用陀螺定向系统有效地抑制了导线横向误差积累。
The working mechanism of the system is quite different from that of the common gyro north-seeking orientating system.
该系统的工作机理与传统的陀螺寻北定向系统有很大的差异。
This paper gives the digital PID control method of the gyro temperature control and introduces the structure and features of a Gyroscope' s temperature test system .
介绍了陀螺数字PID温度控制方法以及陀螺仪温度试验系统的结构和特点，用该系统进行了某型陀螺仪的温度速率试验与位置试验。
By researching and analyzing the system, it is known that the dynamic performance of the gyro bracket and isolation device is the key index of the dynamic performance in the system.
经对系统进行研究分析得知，陀螺仪支架与隔振装置的动态性能是系统动态性能的关键指标。
A new nine-accelerometer configuration of non-gyro inertial measurement unit (NGIMU) is presented, with its experiment system built.
提出了九加速度计无陀螺惯性测量组合(NGIMU)配置方案，并建立了其实验系统。
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