惯性测量系统

基于遥测数据的射前惯性测量系统稳定性检测方法

The Inspection and Measurement of Inertial Surveying System 's Pre-launching Stability Based on Telemetry-data

地地导弹惯性测量系统的稳定性直接影响导弹惯性导航系统导航的准确程度。

The stability of ground-to-ground missile 's inertial surveying system has a direct impact on the accuracy of the inertial navigation system of missiles .

一种基于PC104总线的水下载体惯性测量系统

An Inertial Measurement System for PC 104-based Underwater Carrier

对于由两自由度陀螺构成的冗余捷联惯性测量系统（RSIMS）来说，边缘向量检测（EVT）是一种非常重要和实用的冗余管理算法。

The Edge Vector Test ( EVT ) is a very important and practical redundant management algorithm for Redundant Strapdown Inertial Measurement Sys-tems ( RSIMS ) composed of Two Degree of Freedom gyros .

矿山井下惯性测量系统的仿真研究

Study of the Emulation of Inertial Survey System in Mining Surveying

容错技术在捷联惯性测量系统中的应用

The Application of the Fault-Tolerant Technique to Strapdown Inertial Measurement System

速率捷联惯性测量系统的数学模型及误差标定

Mathematical model and error demarcation of the rate strap-down inertial measuring system

捷联惯性测量系统的误差补偿研究

The Error Compensation Investigation of Strapdown Inertial Measurement System

惯性测量系统测试有效期评估方法研究

Evaluation of Test Valid Period of Inertial Measurement System

弹性体上惯性测量系统的传递对准

Transfer alignment of inertial units on elastic body

微型惯性测量系统及其应用

Micro Inertial Measurement System and its Application

惯性测量系统简化模型的研究

Model Simplification of Inertial Measurement System

惯性测量系统的一种算法

An Algorithm of Inertial Measurement System

惯性测量系统制导精度评估决策支持系统研究

Research on Decision Support System of Guidance Precision Emulation Validating and Evaluation of Inertial Measurement System

捷联式惯性测量系统用于列车实时定位的原理和方法

The principle and method of the high speed train 's real time positioning by strapdown inertial system

速率捷联惯性测量系统

Rate strapdown inertial measurement system

机电技术的发展为惯性测量系统的大量应用奠定了基础。

The development of mechatronic technology laid the foundation for the widely use of inertial measurement systems .

给出了一套弹性体上惯性测量系统的传递对准方案。

An approach to transfer alignment of inertial units on elastic body is proposed in this paper .

随着微惯性测量系统应用的日趋广泛，微小型化是微惯性测量系统发展的重要方向。

With more and more widely used of Micro Inertial Measurement System , micromation is the important developmental direction .

针对惯性测量系统有较大积累误差的缺点，提出了一种向后数值积分算法。

To solve the problem of growth in the error of integration measurement , a backward algorithm is presented .

在以往的惯性测量系统中，常用陀螺测量角速度，而用线加速度计感受线加速度。

Usually in the past inertial measurement systems gyros are used to sense angular velocity and accelerometer for linear acceleration .

作为惯性测量系统的核心，压电陀螺仪的误差直接影响系统精度和性能。

As the essential element of inertial measurement system , the error of piezoelectric gyro affects the accuracy and performance of the system directly .

微加速度计在军事领域的应用包括弹的引信、弹的导航和制导、惯性测量系统和稳定平台。

The application of micro-accelerometer in military area consists of missile fuze , missile navigation , control and guide , inertial measurement system and steady platform .

根据平台式惯性测量系统的实际情况，简化了惯性测量误差模型，推导了平台式惯性测量系统误差观测方程，并进行了车载试验的试验设计。

According to the practice of vehicle test of platform inertial measurement units , the error model of inertial measurement units was simplified , and the error measurement equations were deduced .

由于线加速度计也可以感受角速度，且它的抗冲击能力强、成本低，因此用它来组成无陀螺惯性测量系统具有一定的应用价值。

For accelerometers can also sense angular velocity and bear large impulse with the character of low cost , so the inertial measurement systems based on accelerometers have good application value .

惯性测量系统的测量精度不可能优于对准误差所限定的精度，因此初始对准是捷联惯导系统的研制与应用中一个关键的问题。

The test precision of initial measure system cannot exceed the precision limited by alignment error , so initial alignment is a very important problem in develop and application of the system .

结合舰船甲板动态变形实际情况，在卡尔曼滤波算法的基础上建立了舰船甲板动态变形惯性测量系统的模型，并对该模型进行了仿真。

A model of the ship dynamic deformation inertial measurement system is set up based on Kalman filter algorithm considering the actual situation of ship dynamic deformation , and then makes some simulations for the model .

测斜技术是确定物体在空间的倾斜和倾向的专门技术，它应用于空间飞行器的惯性测量系统、车船体倾斜测量、工程钻孔轨迹检测等许多方面。

Tilt measuring is an expertise that can be used in making sure the incline of the spatial objects . This technology may be applied in many aspects , such as inertia measuring system of spacecraft , incline measuring of vehicle and hull , contrail detecting of broach .

基于Labwindows/CVI的微惯性姿态测量系统设计

Design of the Micro Attitude Measurement System Based on Lab Windows / CVI

微机械传感器的性能分析及其惯性测量装置系统的研究

Performance Analysis of Micro-Mechanical Sensor And Design of Inertial Measure Unit