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。
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。
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。
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。
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。
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。
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。
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 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。
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。
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。
The platform inertial navigation system used peg-top to stabilize the loop through platform and control the angular speed of the platform track navigation coordinate system.
捷联惯导系统利用相对导航坐标系角速度计算姿态矩阵，把雷体坐标系轴向加速度信息转换到导航坐标系轴向并进行导航计算。
The platform inertial navigation system used peg-top to stabilize the loop through platform and control the angular speed of the platform track navigation coordinate system.
捷联惯导系统利用相对导航坐标系角速度计算姿态矩阵，把雷体坐标系轴向加速度信息转换到导航坐标系轴向并进行导航计算。
应用推荐