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two-sample-inertial-algorithm
- 采用经典的双子样算法，实现完整的惯性导航计算。程序中还留有GPS组合导航计算的接口，供开发者进行使用。-Classic two sample algorithm to achieve complete inertial navigation calculations. The program also left interface GPS navigation calculations for developers to use.
inertial-navition
- 基本的惯性导航解算过程以及摇摆条件下的惯性导航程序-Inertial navigation program under the basic inertial navigation solution process and the swing conditions
zuhe
- 对于进行惯性导航过程中对飞机航行导航算法俄验证所需要的惯性数据进行仿真输出-For aircraft inertial navigation process data needed for simulation output
kalmangain
- 该程序用于惯性导航系统误差模型中，求解最优增益，然后用增益引入阻尼。-Kalman filter in INS
INS_trace
- 生成惯性导航原始加计和陀螺数据的matlab仿真程序，位置和角度函数已知并按线性变化，自己可以改成其它函数-raw data of acceleration and angular rate ，INS
GPS-INS
- 1.GPS/INS 组合导航实验仿真 2.包含小的卫星轨道定位、惯性导航定位、卫星GPS定位等程序 3.包括详细的程序说明-1.GPS/INS integrated navigation simulation experiment 2. The satellite orbit positioning contain small, inertial navigation, GPS satellite positioning and other procedures 3. Inclu
SINS-Calculation
- 惯性导航系统精解算程序 -Inertial navigation system-Inertial navigation system calculation
Software
- 惯性导航组合代码,GPS和INS组合代码-software for inertial navigation and gps
dual_2
- 惯性导航系统误差仿真，针对捷联惯导系统的误差方程进行仿真，得到误差曲线-error simulation
Kalman
- 捷联惯性导航，利用卡尔曼滤波，matlab程序，关于初始对准-SINS initial alignment procedure Kalman
matlab-toolbox-forINS
- 惯性导航系统的matlab工具箱，里面包含使用说明以及各个m文件的功能-Inertial navigation system matlab toolbox, which contains instructions for use and various m-file function
Kalman1
- 捷联惯性导航Kalman小失准角精对准程序-SINS Kalman small fine misalignment angle alignment procedure
chunguanxing
- 惯性导航，利用惯性元件（加速度计）来测量运载体本身的加速度，经过积分和运算得到速度和位置，从而达到对运载体导航定位的目的。组成惯性导航系统的设备都安装在运载体内，工作时不依赖外界信息，也不向外界辐射能量，不易受到干扰，是一种自主式导航系统。-Inertial navigation, to measure the carrier itself acceleration Inertial element (accelerometer), through integration and operati
cuduizhun
- 惯性导航系统开始导航之前的工作状态。在此期间，一般进行坐标系对准、初始参数的测定和装定。-Inertial navigation system before starting work state navigation. In the meantime, the general alignment of the coordinate system, initial parameters measured and setter.
CPP
- 几个用C++编写的关于GPS、惯性导航和卡尔曼滤波的程序-Several written in c++ about GPS, inertial navigation and kalman filtering program
transfer-alignment
- 适用于大失准角情形的速度姿态匹 配传递对准非线性误差模型进行惯性导航系统快速传递对准技术研究-For large misalignment angles situation speed Attitude Matching Transfer Alignment nonlinear error model of inertial navigation systems Rapid Transfer Alignment Technology
DirectionCosin
- 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，采用了标准方向余弦法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard method of direction cosine
RotationVector
- 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，采用了标准旋转矢量法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard rotation vector method to s
Euler
- 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，采用了标准欧拉法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard eulerian method to solve the
INS-EKF-master
- 惯性导航 扩展卡尔曼滤波算法 来自于github-Indoor pedestrian location algorithm based on foot-mounted IMU