inertial navigation system是什么意思，inertial navigation system的意思翻译、用法、同义词、例句

[航][水运] 惯性导航系统

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。

The authors think that data from gravity collection system need to be used to compensate or correct errors real-time from gravity aided inertial navigation system in underwater vehicles.

认为水下运动载体的重力辅助惯性导航系统中，其重力数据采集系统为满足导航的需要，必须对重力数据进行实时补偿修正。

The advantages of The FOG Strapdown Inertial Navigation system rest with two aspects: one is that FOG is going to replace the mechanical gyroscope .

光纤陀螺捷联惯导系统的优势在于：一，用光纤陀螺代替了机械式陀螺；

The digital, triple-redundant Lear Siegler flight control system permits coupled automatic terrain following, enhanced by a ring-laser gyro inertial navigation system.

机上的环形激光陀螺惯性导航系统和三余度线传操纵系统能确保飞机做自动地形跟踪飞行。

In order to improve the precision of inertial navigation system, an active filter is designed for filtering the pulsating component induced by nonlinear or unbalanced load in gyroscope power.

以提高惯性导航系统的精度为目的，设计了一种有源滤波器，以滤除陀螺电源中因非线性负载或不平衡负载等造成的电流脉动分量。

The inertial navigation system(INS)error caused by sea current and log error greatly oscillates.

当海况变化较大时，惯性导航系统（INS）的误差振荡幅度较大。

The computer on the strap-down inertial navigation system calculates the location and attitude of the vector, which uses gyro and accelerator as sensor components.

捷联式惯性导航系统以固连在载体上的陀螺组件与加速度组件为敏感元件，利用载体上的导航计算机解算出当前的位置、姿态信息。

The results show that gravity disturbance vector is a major error source for high accuracy inertial navigation system.

结果表明，不确定的重力扰动向量是高精度惯导系统的一个重要误差源。

Without the information transferred by the aircraft, the initial attitude errors would be so large that they become the main errors of the inertial navigation system.

仅依靠有限的信息给惯导系统赋予的初始姿态矩阵误差比较大，初始的姿态误差成为惯导系统的主要误差项。

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。

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。

In the improved curve fitting method, the Schuler component in velocity error was decoupled through the analysis of inertial navigation system.

改进的曲线拟合法通过对惯导系统误差模型的分析，解耦出速度误差项的舒拉部分。

In this paper surrogate-data method of phase-randomized based on correlation dimension is proposed to identify the nonlinearity and chaos of data obtained by ship inertial navigation system.

利用基于关联维数的相位随机化的替代数据法，给出了对船舶运动惯导实测时间序列进行非线性判定和混沌判定的方法。

The cost of the gravity passive inertial navigation system will be lower with a rate azimuth platform and gravity sensor constituting a gravity measurement and navigation system.

为了降低重力无源导航系统成本，在速率方位平台上放置一个重力敏感器，以构成集重力仪和导航仪为一体的系统。

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

无陀螺捷联惯导系统就是惯性元件只用加速度计，而不用陀螺的惯导系统。

The navigation accuracy of the inertial navigation system can be increased greatly by using these techniques, and so that the calibration and the reset period can be extended.

此项技术可以有效地提高惯性导航系统的导航精度，并可大幅度地延长校准和重调周期。

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

由于捷联惯导系统具有的一系列优点，在许多应用中有取代平台式惯导系统的趋势。

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。

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。

In this paper, the low-cost SINS/GPS integrated navigation system, which consists of inertial navigation system and global position system, is designed and Real-time simulated.

本文进行了低成本SINS/GPS组合导航系统的仿真与实时软件设计。此组合系统由惯性系统和GPS系统构成。

Improving the accuracy of angular resolution is the key way to improve the navigation parameter resolution precision of accelerometer based gyro-free inertial navigation system.

提高角速度解算精度是提高无陀螺惯性导航系统导航参数解算精度的主要途径。

The attitude, velocity and position differential equations of Strapdown Inertial Navigation System (SINS) for the design of SINS algorithm were introduced.

针对捷联惯导系统（SINS）的算法设计，介绍了SINS的姿态、速度和位置基本微分方程组；

In the thesis, the technology of initial alignment and transfer alignment of the inertial navigation system of the carrier borne plane when the aircraft carrier is moored or is cruising is researched.

本文以舰载机为研究对象，系统全面地研究了其惯导系统在航母系泊和巡航条件下的初始自对准技术和传递对准技术。