Gyroscope static drift coefficient of inertial platform can be separated wholly by using the method.
该方法可完整地分离出惯性平台陀螺仪各项静态漂移系数。
This paper presents a method to calibrate gyro drifts on inertial platform using output of accelerometers.
本文给出了利用加速度计输出标定惯性平台陀螺漂移的方法。
So, the data interface between data processing computer and inertial platform is important for survey system.
为此，从惯性平台到数据处理计算机的接口是很重要的。
These methods are very helpful to error separation of inertial platform systems or Position Strap-down systems.
此方法对平台系统或位置捷联系统的误差分离具有较重要的参考价值。
This paper discusses the design problem of the variable structure sliding mode control for the inertial platform stabilizing circuits.
本文讨论了惯性平台稳定回路的变结构滑模控制规律的设计问题。
This paper discusses the design problem of active disturbance rejection control (ADRC) for the inertial platform stabilizing circuits.
讨论了惯性平台稳定回路自抗扰控制的设计问题。
The identification result of the gyro misalignment angle in inertial platform is unsatisfactory for the static multiposition test scheme.
在惯导平台多位置静态测漂方案下，对陀螺安装误差角的辨识结果往往很不理想。
Inertial positioning system, in which an inertial platform has three mutually perpendicular axes, one of which is "up", so that the system yields elevation as one of the outputs.
惯性定位系统，在惯性平台有三个互相垂直的轴，其中之一是“上”，使系统产生海拔为一体的输出。
One of the approaches in the enhancement of accuracy of inertial platform is to perform the realtime compensation of the systematic component of platform's error by use of computer.
提高惯性平台使用精度的途径之一是用计算机实时补偿平台误差的系统分量。
The flight trim aerodynamic characteristics of re-entry modules were calculated from on board-recorded inertial-platform accelerations and attitudes and from reconstructed trajectory data.
返回舱飞行试验的配平气动特性可从舱内惯性平台的加速度和姿态记录数据以及轨道数据求出。
Because the real input acceleration can not be obtained during the error model identification of the inertial navigation platform, so the measurement value is used to substitute the input data.
在进行惯导平台误差模型辨识的过程中，真实的输入加速度难以获得，因此不得不使用测量值来代替，这使得输入输出观测数据中均含有测量噪声。
According to symmetry, at arbitrary degree of freedom, inertial stabilization platform was simplified to one degree of freedom.
根据对称性，在任意一个自由度方向将惯性稳定平台简化为单自由度系统。
The stabilization of the platform determines the precision of INS, while the platform stabilization loop forces the platform to the inertial space.
平台的稳定性直接影响导航系统的精度，而平台稳定回路则担当了将平台稳定在惯性空间的任务。
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。
The structures and principle of a miniaturized inertial control platform were described in this paper.
简述了小型惯性控制平台的组成和工作原理，运用动力学原理建立了台体结构模型。
In this paper, an engineering example of drift error parameter identification for a type of inertial navigation platform is presented.
本文给出了某型号惯导平台漂移误差参数辨识的一个工程实例。
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。
In this paper, the parameter identification technique of inertial navigation platform drifting error model is studied.
本文研究了惯导平台漂移误差模型的参数辨识技术。
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.
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。
The airborne SAR (Synthesis Aperture Radar) USES a stabilized platform to make the antenna stable in the inertial place and trace the velocity to the ground.
机载合成孔径雷达使用陀螺稳定平台使天线在惯性空间保持稳定并跟踪地速方向。
The inertial system of fighting vehicle existed bracket error due to its two-axis gyro platform structure, and this could influence the heading precision.
战车用惯性定位定向系统由于采用双轴陀螺平台结构，不可避免地存在着支架误差，从而影响系统航向精度。
PWM control system for the temperature of inertial navigation platform with single chip microcomputer is described in this paper.
本文介绍了惯导平台温度的单片机p WM控制系统。
This paper presents a new continuous self-calibration and alignment technology of inertial navigation platform.
提出了一种新的惯导误差系数标定方法———连续自标定自对准方法。
Main reasons for heading effect drift of an airborne platform inertial navigation system are analyzed in this paper.
文中分析了某型平台式惯性导航系统航向漂移产生的主要原因。
The inertial navigation technology includes platform inertial navigation system and SINS.
包括平台式惯导系统和捷联惯导系统。
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。
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。
This can detect the position of platform feed with great inertial-mass through photoelectrical encoder, the vibration magnitude of translation worktable with eddy transducer.
用光电编码器实现了大质量进给滑台的位置检测；
The paper introduces a new experience platform which is based on the combination of the augmented reality technology, strapdown inertial navigating system and force-feedback technology.
本文介绍了一个结合增强现实、惯性导航和力反馈技术的体验平台。
The paper introduces a new experience platform which is based on the combination of the augmented reality technology, strapdown inertial navigating system and force-feedback technology.
本文介绍了一个结合增强现实、惯性导航和力反馈技术的体验平台。
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