inertial navigation system
美 
英
- 网络惯性导航系统；惯性导航系统惯导系统；惯性导航装置
例句
The attitude solution for carrier is one of the key technologies for precision navigation of Strapdown Inertial Navigation System(SINS).
载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一。
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。
Avionics systems include a highly accurate inertial navigation system in which a computer provides steering information to the pilot.
航电系统包括高度精确的惯性导航系统，它通过电脑向飞行员提供转向信息。
Main reasons for heading effect drift of an airborne platform inertial navigation system are analyzed in this paper.
本文分析了某型机载平台式惯性导航系统航向效应漂移产生的主要原因。
Inertial navigation system is composed of strap down inertial navigation system and platform inertial navigation system.
惯性导航定位系统分为平台式惯导系统和捷联式惯导系统两种。
An online identification algorithm of odometers scale factor in land used strapdown inertial navigation system is put forward.
提出陆用捷联惯导系统中里程计刻度因子的在线辨识算法。
In the paper, the scrolling compensation algorithm in position updating of strap down inertial navigation system is researched.
研究了高动态环境下捷联惯导位置更新中的涡卷补偿算法。
Inertial Navigation System (INS) is a important navigation system with widely application in civil and military field.
惯性导航系统（INS）是一种非常重要的导航定位系统，在民用和军事领域有广泛的应用。
Strapdown Inertial Navigation System (SINS) leads the trend of inertial navigation systems currently.
捷联式惯性导航系统（SINS）是目前惯性导航技术的主要发展方向。
This paper discussed and researched strap down inertial navigation system used in rock oil pipeline detection based on project practice.
本论文以实际的工程为背景，主要讨论并研究了捷联式惯导系统在石油管道检测中的应用。
The digital levelling and fast accurate levelling method for strap down inertial navigation system (SINS) is discussed.
讨论了实现捷联惯导系统数字调平及快速精调平的方法。
It could be used in the closed-loop simulation test of flight control system and inertial navigation system.
它可用于飞行控制系统与惯性导航系统的标定和闭环仿真实验。
Strap down inertial navigation system is a developmental orientation of inertial technique.
捷联式惯导系统是近年来惯性导航技术的一个发展方向。
Compared with Platform Inertial Navigation System, SINS is smaller in size, lighter in weight, more reliable and cheaper.
它与平台式惯性导航系统相比具有体积小、重量轻、成本低、可靠性高等诸多优点。
and coning error from coning motion is an essential error source of strap down inertial navigation system(SINS).
在圆锥运动下产生的圆锥误差是捷联惯导系统的重要误差源。
Initial Alignment of Inertial Navigation System Using Wavelet Neural Networks.
采用小波神经网络的惯导系统初始对准。
Finally, the block diagram of the strap-down inertial navigation system is given .
最后给出了无陀螺捷联惯性导航系统的框图。
The parameter error of inertial navigation system has important effect on the precision of navigation system.
捷联惯性导航系统误差参数标定的准确程度对于系统的导航和定位精度具有重要影响。
An expert system is proposed to diagnose faults of platform inertial navigation system.
分析了导航系统对故障诊断的基本要求以及导航系统的故障诊断方法。
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。
A new type of inertial navigation system combining customary platform type with strap-down one is put forward.
本文提出一种把平台式和捷联式惯导系统结合在一起的新的惯性导航系统。
The strap down inertial navigation system(SINS) in weapon system needs initial alignment before the weapon is launched.
目前远程武器系统广泛采用捷联惯性导航系统，该系统在发射前要经过初始对准。
A inertial navigation system, this module includes forward back pluse signals, the gyro signal, speed pulse signal and the barometer signal.
提出了一种递推导航方案，此方案包括了前后向信号、陀螺仪信号、速度脉冲信号以及气压计信号。
The method of integrated attitude determination based on inertial navigation system and star sensor is researched in this paper.
研究了利用惯性导航系统与星敏感器进行组合定姿的方法。
With the development of the ship and navigation, the inertial navigation system shows its more and more important status.
随着船舶和航海事业的日益发展，惯性技术越来越显示出其重要的地位。
In order to utilize it better in the new generation inertial navigation system, it is necessary to study the random error model of VBA.
为了更好地将振梁加速度计应用于新一代惯导系统中，有必要研究其随机误差模型。
Study of Time Synchronization of Simulation on Strapdown Inertial Navigation System
捷联惯导系统半实物仿真试验的时序同步研究
A Real- time Neural Network Learning Algorithm Adapt to the Initial Alignment of Inertial Navigation System
适于惯导系统初始对准的神经网络实时算法研究
Generalized Inferential Control Strategy for Expert System and its Application in Inertial Navigation System
专家系统的广义推理控制策略研究及其在惯导系统中的应用
Study of Self-Calibration Technique for Sensor Errors in Ring Laser Gyro Strapdown Inertial Navigation System
激光陀螺捷联惯导系统元件误差自标定技术
Application of Two-position Alignment Technique in Strapdown Inertial Navigation System for Land Vehicle
双位置初始对准技术在车载捷联惯导系统中的应用研究
Multiposition Observability Analysis of Strapdown Inertial Navigation System
捷联惯导系统多位置可观性分析
Initial Alignment Accuracy Analysis and Simulation of Strapdown Inertial Navigation System on a Stationary Base
捷联惯导系统静基座初始对准精度分析及仿真
Research on a Fast Initial Alignment Method for the Strapdown Inertial Navigation System on Stationary Base
捷联式惯导系统静基座快速初始对准方法的研究
Inertial Instrument Error Compensation Technology in Laser Gyro Strapdown Inertial Navigation System
激光陀螺捷联惯性导航系统中惯性器件误差补偿技术
Study on noncommutativity errors correction algorithms of laser strapdown inertial navigation system
激光捷联惯性导航中不可交换性误差补偿算法研究
Fast Initial Alignment and Its Errors of RLG Strapdown Inertial Navigation System for Land Vehicle
车载激光捷联惯导系统的快速初始对准及误差分析
Initial alignment of the inertial navigation system based on a neural network suitable for the best estimation
基于最优估计神经网络的惯导系统初始对准研究
Coupled Vibration Characteristics of Strapdown Inertial Navigation System
捷联惯导系统振动耦合特性研究
Application of Active Disturbance Rejection Technique in Initial Alignment of Inertial Navigation System
自抗扰控制在惯性导航系统初始对准中的应用
