inertial navigation

1. Research on Initial Alignment of Fiber-Optic Gyroscope Inertial Navigation System
   光纤陀螺捷联惯导系统初始对准技术研究
2. Polynomial smoothing method is used for preprocessing the dynamic data of Inertial Navigation System ( INS). By using the method, the influence of various noises on data processing is decreased.
   采用多项式平滑方法对惯导系统的动态数据进行预处理，降低了各种噪声对数据处理的影响。
3. Application of the extend state observer on the initial alignment of the inertial navigation system
   扩张状态观测器在惯导系统初始对准中的应用研究
4. Research and Analysis on Error Caused by Lever Arm Effect in Platform Inertial Navigation System
   平台惯导系统中杆臂效应误差的研究与分析
5. Based on the Global Positioning System ( GPS) software receiver and Strapdown Inertial Navigation System ( SINS) aiding GPS tracking technology, SINS/ GPS ultra-tight integration scheme is presented.
   在GPS软件接收机和SINS辅助GPS跟踪技术的基础上，提出了一种SINS/GPS超紧致组合导航方案。
6. Secondly, the principle of strap down inertial navigation for a rocket or cannon artillery is analyzed in details.
   进而讨论了针对火箭炮或身管火炮的捷联惯性导航原理。
7. Instrument Error Calculation and Compensation of Rate Strapdown Inertial Navigation System
   速率捷联惯导系统工具误差计算与补偿研究
8. Power spectrum analysis for laser gyro damping system of strapdown inertial navigation
   激光陀螺捷联惯导系统减振功率谱分析
9. Analysis of Gravity Field Effect on High-precision Inertial Navigation System
   高精度惯性导航系统的重力场影响模式分析
10. Research of Integrated Navigation System Based on Strapdown Inertial Navigation System
    基于捷联惯性导航的组合导航系统研究
11. Global positioning system real time kinematic technology ( GPS RTK) was applied to the error model identification of the inertial navigation platform in this paper.
    对在惯导平台车载试验误差模型辨识中使用全球卫星定位系统（GPS）载波相位差分（RTK）法进行了研究。
12. The principle of equivalence is of critical importance in our analysis of inertial navigation.
    等效原理在惯性导航分析中特别重要。
13. Error Compensation Methods for Inertial Navigation System in Deep Sea
    深海环境惯性导航系统误差补偿方法的研究
14. Finally, the control law is applied to the inertial navigation system and its feasibility is studied and verified in the simulation experiment.
    最后，对该方法在惯性导航系统中的应用进行了仿真研究，验证了其可行性和有效性。
15. Research on Optimal Attitude Algorithm of 3-Subsample Rotation Vector in Strapdown Inertial Navigation System
    三子样旋转矢量优化姿态算法在捷联惯导中的研究
16. 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。
17. Application of Virtual Instrument Technology in Strapdown Inertial Navigation System
    虚拟仪表在捷联惯导系统中的简单应用
18. The Design of Inertial Navigation System Simulator Based on Submarine Space Motion
    基于潜艇空间运动的惯性导航系统模拟器设计
19. In this paper, the continuous automatic calibration technology of laser gyro strapdown inertial navigation system is studied.
    本文研究的是激光陀螺捷联惯导系统的连续自动标定技术。
20. In scene matching aided navigation system, excursion of inertial navigation system and measurement error of wireless pressure altimeter cause the distortion between query image and reference image.
    在景象匹配辅助导航系统中，惯性导航系统的漂移和无线电气压高度表的测量误差使得实测图和参考图之间产生了变形。
21. Depending on the error analysis of the strap-down inertial navigation system, the error equation of this system is given.
    在分析捷联系统误差的基础上，给出了系统的误差方程。
22. Improved FOG Strapdown Inertial Navigation System and Error Analysis
    旋转光纤捷联惯性导航系统的误差调制分析
23. Methods of error compensation for azimuth holding system in an INS ( inertial navigation system) are presented.
    给出了陆用惯性导航系统方位保持仪的误差补偿方法。
24. A new fusion algorithm of the measurements from global positioning system ( GPS) and inertial navigation system ( INS) is presented to compensate the weaknesses of current integrated navigation system.
    为了弥补现有组合导航算法的不足，提出了一种新的GPS量测数据和惯性导航系统（INS）数据的融合算法。
25. Research on Integrated Navigation and Zero Velocity Update Technology of Strapdown Inertial Navigation System with Ring Laser Gyroscope
    激光陀螺捷联惯性导航系统组合导航及零速修正技术研究
26. Simulation and test results of a laser gyro strapdown inertial navigation system show that the improved calibration scheme can increase the calibration accuracy and improve the navigation performance.
    仿真和试验对标定编排改进前后的标定精度和导航性能进行了对比，表明改进编排方案可以提高陀螺和加速度计安装误差角标定精度，改善系统导航性能。
27. The simulation results indicate that the calibration can compensate the error and improve the precision of the inertial navigation system.
    仿真结果表明，该标定方法能够对误差进行补偿，进而提高惯导系统的导航精度。
28. The discussion focuses on the ESG's drift model and its compensation as well as monitoring in a inertial navigation system.
    着重讨论静电陀螺漂移模型及其在系统中补偿和监控方法。
29. This area of study is central to the technology of inertial navigation and gyroscopic stabilization.
    这个研究领域是惯性导航和陀螺稳定器技术的核心。

noun

1. a method of controlling the flight of a missile by devices that respond to inertial forces

   Synonym:    inertial guidance