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mine2
- 捷联惯导系统导航解算. 根据600秒的指北方位捷联系统的数据进行导航解算，飞行高度不变，采样周期0.01s.-Strapdown inertial navigation system navigation solution. Based on the 600 seconds that the north-bit data SINS navigation solution, the same altitude, sampling period 0.01s.
test2
- 捷联更新 matlab 仿真 捷联惯导 控制导航-Strapdown update matlab simulation SINS control navigation
Sfangzhenshujt
- 捷联惯导系统仿真数据生成工具，，可以用来验证捷联算法可直接使用。 -SINS simulation data generation tool that can be used to verify that the strapdown algorithm can be used directly.
Direct
- dBasic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is established, and its Matlab implement
Direct_C_Noise
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is established, and its Matlab implementat
GEN
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is established, and its Matlab implementat
Indirect_Cancel
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is established, and its Matlab implementat
Yan-Gong-Min-_-PhD-thesis
- 严恭敏_博士学位论文 论文中采用激光陀螺捷联惯导系统为主导航系统，通过与里程计和气压高度计组合，构成车载自主定位定向系统，并借助路标点进行误差补偿。该定位定向系统不依靠 GPS，中途无须停车作零速修正，是一种全自主的导航系统，具有定位定向精度高、机动性好、可靠性高和寿命长等优点。 -In this thesis, laser gyro strapdown inertial navigation system (SINS) is selected as core navigation s
KF
- 初始对准是捷联惯导系统进行导航的前提，初始对准的好坏将直接影响到系统的导航精度。捷联惯导系统(SINS)初始对准的本质是确定载体的初始姿态。-The initial alignment of strapdown inertial navigation system is the premise for navigation, initial alignment will directly affect the quality of the navigation system precision.
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
- 使用C语言写的捷联惯导解算程序，四子样旋转矢量-Using C language to write the strapdown inertial navigation program, four sample rotation vector
KF_SINS
- 本程序为捷联惯导系统静基座对准卡尔曼滤波程序，观测量为水平速度误差，程序经本人验证正确无误。(This program is a static mount of strapdown inertial navigation system (SINS). It is a Calman filtering program, and the observation is horizontal velocity error. The program is proved correct by myself.
chuandiduizhun
- 捷联惯导系统传递对准matlab程序,已经验证过，非常好用(matlab sins Transfer alignment of strapdown inertial navig)
sins
- 捷联惯导的详细介绍，附有编程程序供大家参考学习(Strapdown inertial navigation system in detail, with programming procedures for your reference learning)
捷联惯导及其组合导航研究
- 本文对捷联惯导系统(sINS)及其与全球定位系统(GPS)的组合导航系统进行 了研究。首先对实现S取S的初始对准及姿态矩阵计算等关键技术进行了系统研究。 在仿真的基础上进行了实际捷联惯导系统的系统研制，针对陀螺漂移补偿等关键算法 开展深入研究，实验结果表明经过补偿解算后，整个捷联惯导系统导航参数的解算精 度大大提高。在实现SINS的基础土，研究了SINS与GPS(The strapdown inertial navigation system (sINS) and global posi
SINS
- 捷联惯导算法、四元数算法姿态解算、误差补偿及仿真分析，matlab仿真程序(Attitude calculation of strapdown inertial navigation system algorithm based on Matlab)
GPS_SINS
- 几个用C++编写的关于GPS捷联惯性组合导航的程序，采用kalman滤波(Several programs written in C++ about GPS strapdown inertial integrated navigation, using Kalman filtering)
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)