• 包括平台式系统捷联惯导系统。

    The inertial navigation technology includes platform inertial navigation system and SINS.

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  • 姿态算法研究

    Study on attitude-updating algorithm.

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  • 本文设计了型飞机捷联姿计算机硬件系统

    In this paper, the hardware of a strap-down heading and attitude computer is designed.

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  • 因此初始对准捷联惯导系统重要关键技术之一

    So the original alignment is one of the most important key technical of the INS.

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  • 捷联惯导系统中,数学平台代替了常规物理平台。

    IN SINS system, physical platform of traditional INS is replaced by mathematical platform.

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  • 捷联惯导系统中,数学平台代替了常规物理平台。

    IN SINS, physical platform of traditional INS is replaced by mathematical platform.

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  • 提出惯导系统里程刻度因子在线辨识算法

    An online identification algorithm of odometer's scale factor in land used strapdown inertial navigation system is put forward.

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  • 惯导技术军事和国民生产诸多领域有着广泛的应用。

    Strapdown inertial navigation technology has been widely used in military and national production.

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  • 我们相信男子处以自己捷联惯导系统不是亚当海侵

    We believe that men will be punished for their own SINS, and not for Adam's transgression.

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  • 陀螺系统就是惯性元件只用加速度计不用陀螺惯导系统。

    So-called GFSINS (gyroscope free strapdown inertial navigation system) is a kind of strapdown inertial navigation system with only accelerometers but no gyroscope.

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  • 分别讨论平台罗经垂直参考基准提供摇摆数据前馈稳定实现方法

    Discuss the methods to provide rock data of feedforward of gyrocompass and strap-down inertial system.

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  • 工程实用维护角度出发,提出一种针对机载捷联式系统空中标定方法

    In view of engineering utility and maintenance, an in-flight calibration method for aircraft SINS was presented.

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  • 忏悔我们应该承认这些捷联惯导系统我们知道觉得我们的心中

    But before the confessor we should confess those SINS alone which we know and feel in our hearts.

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  • 圆锥误差量化误差激光惯性导航系统姿态解算误差两个最主要的误差源。

    Coning error and quantizing error are two kinds of primary errors in the attitude algorithm of laser strap-down inertial system.

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  • 由于惯导系统具有一系列优点,许多应用中有取代平台式惯导系统的趋势

    Because of these advantages of SINS system, it is on the trend of replacing flat inertial navigation system in many applications.

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  • 针对惯导系统基座初始对准问题,提出一种新的动基座快速传递对准方案

    A new approach to transfer alignment for the initial alignment of Strapdown inertial navigation systems on moving base was put forward.

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  • 数十年来,元数及其解法成功地应用惯性导航制导系统中,成为经典的算法。

    Quaternion method, which has been successfully applied to the Strapdown Inertial Navigation and Guidance for tens year, is classical.

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  • 实验仿真结果表明无陀螺捷联系统相比组合导航系统精度容错性能显著提高

    Computer simulation results show that, the precision and fault tolerance of the integrated navigation system are improved greatly, compared with the pure GFSINS.

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  • 本文主要针对车载捷联惯导系统快速性反应一要求,研究了车辆动机座初始对准方法问题。

    The initial alignment of vehicle in moving state is studied mostly in this paper aiming at fast response of the vehicle carried SINS.

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  • 惯导系统中,可以四元数表示姿态矩阵姿态矩阵计算捷联导系统关键问题之一。

    Attitude matrix is represented by quaternion and the calculation of attitude matrix is a key in Strapdown INS.

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  • 文章基于变换原理,结合待测信号特点,创造性地提出一适用仪的小波消噪

    Base on wavelet denoising theory as well as the characteristic of the signal, a wavelet denoising method applied to Strapdown north seeking system was proposed.

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  • 介绍了惯导系统数字基本原理实现过程然后讨论了通过数据周期延拓实现快速调平的方法。

    The theory and realizing process of digital levelling for SINS is introduced, then fast accurate levelling method by data cyclic continuation is discussed.

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  • 详细描述了惯性导航系统(SINS)中加速度计陀螺数据仿真方法给出了求解扰动重力算法

    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.

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  • 着重研究了隔离环稳定回路的一种校正方案,通过采用超前滞后网络横滚隔离光纤惯导稳定回路进行校正。

    The approach is called lead and lag correction which has been adopted to correct the stabilization loop of roll-isolated fiber optical gyro strap-down inertial navigation system (RIFOGSINS).

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  • 详细研究不同机动方式机载武器捷联惯导系统传递对准性能影响计算机仿真结果进行深入分析

    Detailed investigation of different maneuver manners effect on the performance of SINS transfer alignment and in-depth analysis of the simulation outcomes were carried out.

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  • 详细研究不同机动方式机载武器捷联惯导系统传递对准性能影响计算机仿真结果进行深入分析

    Detailed investigation of different maneuver manners effect on the performance of SINS transfer alignment and in-depth analysis of the simulation outcomes were carried out.

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