搜索资源列表
SINS-MATLAB-simulation-program-source-code
- 捷联惯导仿真程序MATLAB源代码，能帮助大家了解捷联惯导原理-SINS MATLAB simulation program source code, can help you understand the principles of the SINS
strapdown
- 自编的SINS仿真Matlab程序，对初学者还算全，应该有点用处，虽然比较简单，也省些前期编写的麻烦-The SINS self-compiled Matlab simulation program, for beginners fairly full, it should be somewhat useful, though relatively simple, but also save some trouble of pre-prepared
GPSSINSNavigation
- matlab 编写的gps/sins组合导航程序,附程序说明与数据输入文件-matlab prepared gps/sins navigation procedures, with explanation of the procedures and data input file
strap_down_inertial_navigation
- 捷联系统C语言实现算法，已经过实验验证。-SINS C language algorithm, has been verified by tests.
matlab
- matlab应用于捷联惯导系统初始对准滤波技术程序-matlab applies SINS initial alignment procedures Filtering Technique
INSandGPS
- 捷联惯导GPS组合导航Kalman滤波器-SINS GPS Navigation Kalman Filter
MatlabofSINS
- SINS仿真Matlab程序，对初学者还算全，应该有点用处，虽然比较简单，也省些前期编写的麻烦， 希望能花更多时间研究些专门的有用处的东西。如大家有需要还可增加一些其它内容-SINS Matlab simulation program, for beginners fairly full, should be of some use, although relatively simple, but also save the trouble of some pre-prepared, I h
another
- 复杂捷联惯导的另一种解算方法，包括解算位置、速率与姿态-Complex SINS another solution method, including calculating position, velocity and attitude
SimulationSINS
- 基于四元数法的捷联惯导系统仿真，陀螺仪和加速度计数据为自己仿的一分钟数据-Simulation SINS
EKF_5order
- EKF在捷联惯性导航系统初始对准中的应用？在方位角为大失准角的情况下，如何进行初始对准-EKF in SINS Initial Alignment? In the azimuth misalignment angle for the big cases, how to initial alignment
SINS-MATLAB
- 捷联惯导（SINS）的MATLAB仿真程序-SINS of the MATLAB simulation program
SINS-Alignment(matlab)
- 捷联惯导初始对准的程序 matlab写的 包括动基座和静基座对准。-Initial Alignment of SINS program written in matlab, including dynamic and static alignment.
MATLAB-sins
- 利用matlab编写的捷联惯导程序，可以做参考，参考价值大-Prepared using matlab SINS program, you can do reference, reference-value
Attitude-SINS
- 姿态角仿真 MATLAB 捷联惯导 三阶泰勒 四阶龙格库塔-MATLAB simulation Attitude SINS fourth order Runge-Kutta third-order Taylor
a-new-method-for-moving-SINS
- 本文在运载体运动情况下，提出了一种适用于捷联惯导系初始对准的新算法，该算法以 惯性空间为参考基准，将初始对准姿态矩阵的实现分解为三部分-This movement of the transporter, the paper presents a system for SINS Initial Alignment of the new algorithm to inertial space as the reference point, the realization of initial a
sins-matlab
- 捷联惯导系统的matlab程序源代码，包含输出代码，非常好用-The SINS matlab program source code, including the output code, it is very easy to use
SINS-matlab-solver-
- 压缩文件包含两部分，一部分为捷联惯导的基本内容，是.ppt，一共五章。还有一部分为捷联惯导的解算程序，共九个，是.m文件。用的时候需要将数据的txt文档放在文件夹内，运行test.m即可。-The compressed file contains two parts, one for the sins of the basic ppt, a total of five chapters. SINS solver, a total of nine, is the m files. Used whe
SINS
- 捷联惯性导航系统中，利用四元数法进行状态变量估计~并运用到SINS/GPS组合导航系统中~-Strapdown inertial navigation system, using the quaternion method the state variables estimated ~ and applied to the SINS/GPS Integrated Navigation System ~
InitialAlignment
- 采用最小二乘估计和Kalman滤波估计方法，提出、设计实现了一个有效实用的FOG 捷联式惯导系统（SINS）初始对准方法。-the least twin multiplication estimatin The Kalman filter estimation are adopted, and a FOG SINS’s initial alignment method is put foreword and designed.
Design-and-Analysis-of-GPS-SINS-Integrated-System
- A very good paper describing the detail of SINS and GPS integration