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基于Kalman滤波的惯性导航
- 基于Kalman滤波的惯性组合导航
INS_GPS
- INS_GPS导航中联邦卡尔曼滤波算法 INS_GPS导航中联邦卡尔曼滤波算法-INS_GPS federal navigation Kalman filter algorithm INS_GPS federal navigation Kalman filter Algorithm
differential_GPS_INS_navigation
- 这是针对差分GPS和惯性导航的组合导航技术的研究论文,有较高的理论研究和工程参考价值.-This is for differential GPS and inertial navigation technology, a combination of navigation research papers, have a higher theoretical research and engineering reference value
Power-assistcaj
- 水下运载体重力辅助惯性导航系统仿真平台的建立-Power-assisted delivery weight underwater inertial navigation system simulation platform for the establishment of
GPS_INS0914
- 捷联惯性导航与GPS组合导航。采用matlab实现。采用自适应算法对其进行处理。并取得了很好的效果。-Strapdown inertial navigation and GPS Navigation. Using matlab to achieve. Adaptive algorithm used to deal with them. And has achieved good results.
RtwMatrix
- GPS惯性导航系统,解压后会有5M,这是我利用C#针对嵌入式WinCE做的一个GPS/惯性导航系统的组合定位软件，包括了卡尔曼滤波算法（含矩阵控件），界面显示，GPS串口接受，滤波结果输出以及WinCE应用调试控件，超强吧！直接下载可以在Visual.Net下调试使用-GPS inertial navigation system, after decompression will be 5M, which I use C# for em
惯性导航四元数法
- 主要利用四元数来解算姿态角，并实时更新四元数，然后实时更新姿态角。(The attitude angle is calculated by four variables, and the four variables are updated in real time, and then the attitude angle is updated in real time.)
惯性导航中加速度计和陀螺仪性能研究_徐东升
- 通过利用陀螺仪数据来解算和更新四元数，进而来计算姿态角。(The attitude angle is calculated by using the gyro data to solve and update the number of four variables.)
Factor Graph in Inertial Navigation Systems
- 利用因子图和积算法设计的无人机惯性导航系统算法，利用matlab仿真实现(An algorithm of unmanned aerial vehicle (UAV) inertial navigation system designed by factor diagram and calculation method is realized by MATLAB simulation)
INSNEW
- 根据给定的数据进行惯性导航的解算，从而确定姿态，速度和位置的更新(The calculation of inertial navigation based on the given data to determine the update of attitude, speed and position)
天文惯性组合仿真软件程序version2.1
- 天文惯性组合导航软件仿真程序，供参考。(Software simulation program for astronomical inertial integrated navigation)
矩阵论例题
- 惯性导航MATLAB程序，里面涉及到四元数算法(Inertial navigation MATLAB program)
1111.tar
- 捷联惯性导航技术（第2版）,非常不错的东西，值得一看(Gemini's inertial navigation technology (version 2), very good stuff, worth seeing.)
crazyfile
- 捷联式惯性导航系统姿态结算，可以得出pitch（y轴）和roll（x轴） 方案为：stm32+mcu6050(Inertial navigation system attitude settlement can be drawn pitch (y-axis) and roll (x-axis) Solutions for: stm32+ mcu6050)
SINS-MATLAB
- 惯性导航程序,matlab程序, 有注释,很不错的参考程序(strapdown navigation matlab code)
D4
- 一个简单的惯性导航模拟实现，实现计算姿态角，速度和经纬高的功能(A simple implementation of inertial navigation simulation to calculate attitude angle, velocity and latitude-longitude height)
tra011
- 惯性导航解算，得出飞行器的经度纬度高度，陀螺仪和加速度计的值(Inertial Navigation Solution, the longitude, latitude, altitude, gyroscope and accelerometer of the aircraft are obtained.)
书籍电子版
- 包含GPS导航原理与 应用 Kalman滤波理论及其哎导航系统中应用 秦永远的惯性导航，以及严恭敏的捷联惯导与组合导航原理讲义(Including GPS navigation principle and application Kalman filtering theory and its application in navigation system Qin Yong's inertial navigation, and
捷联惯导算法与组合导航原理讲义(20190410)
- 本书是作者在总结多年研究生“卡尔曼滤波与组合导航原理”课程的教学经验，吸收十余年从事惯性导航与组合导航技术研究的科研成果，以及参阅国内外众多文献资料的基础上编写的，注重基础理论与工程实践相结合，实用性与可操作性强。全书共八章，主要包括捷联惯导算法及其误差分析、地球重力场基础、卡尔曼滤波基本原理、初始对准与组合导航技术、捷联惯导与组合导航仿真等内容。书中附有丰富的Matlab仿真程序可供参考，还有练习题可供读者拓展学习或学生练习使用。(I
惯性测量装置IMU的仿真模型
- 惯性测量装置IMU的matlab仿真模型。(Matlab simulation model of IMU.)