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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
SINS-Calculation
- 惯性导航系统精解算程序 -Inertial navigation system-Inertial navigation system calculation
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
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
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.
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
AHRS
- 捷联式惯性导航，四元素解析姿态。用基本的C程序完成。可移植性高。惯性导航系统。但是里程计还没做好。 值得学习-Strapdown inertial navigation, four element analytic posture.With the basic C program to complete.High portability.Inertial navigation system.But the odometer is not ready. Worth learning
Matlab-INS-toolbox
- 该惯性导航系统工具箱（INS）就是专门为这个目的设计的。这个工具箱可以用来模拟仿真载体动力学，处理原始测量值（加速计上的delta-V数据和陀螺仪上的delte-theta数据）和数据。-The inertial navigation system (INS) is specially designed for this purpose. The kit can be used to simulate carrier dynamics, processing raw measurements (
psins151009
- 高精度捷联惯性导航系统Matlab工具箱：姿态向量、四元数、矩阵、滤波算法等各类子程序- High-precision inertial navigation system Matlab toolbox: attitude vector, quaternion, matrix, and other types of filtering algorithm subroutine
SINS
- 捷联惯性导航系统的matlab仿真，还包含圆锥误差的补偿等。-Matlab simulation of strapdown inertial navigation system, including the compensation of the error of the cone, etc..
SINS-Matlab
- SINS，捷联惯性导航系统，是目前一种主要的惯性导航系统，在飞机、导弹以及航天器上，多有应用，这里提供惯性导航系统仿真程序，以方便大家使用参考-Matlab for SINS
IEZ
- 惯性导航系统,INS,step_detection,ZUPT(PDR , pedestrian navigation system)
mutisencer navgation
- GNSS与惯性及多传感器组合导航系统原理（第二版）-光盘资料(GNSS and inertial and multi-sensor integrated navigation system principles (Second Edition) - CD-ROM data)
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- 简单实用的捷联惯导系统，附有注释详解，适合初学者(Simple and practical strapdown inertial navigation system, annotated with detailed explanations, suitable for beginners)
光纤陀螺随机漂移的建模_分析和补偿
- 光纤陀螺是基于效应工作的角速率传感器，具有全固态、体积小、 质量轻、动态范围宽、启动快、成本低、易集成等突出特点，在军事和民用领 域备受世界各国关注，获得了广泛应用。然而，受元器件性能、寄生效应和周 围环境的影响，光纤陀螺的输出易产生漂移，影响惯性导航系统的精度。因此， 抑制光纤陀螺漂移误差，提高其测量精度具有重要意义。(Fiber optic gyroscope(FOG) is a kind of angular rate sensor based on Sagnac erect w
guandao123456
- 对于惯性导航系统的matlab仿真，适合与最基础的仿真学习(Matlab simulation for inertial navigation system, and for the most basic simulation study)