搜索资源列表
INSandGPS
- 捷联惯导GPS组合导航Kalman滤波器-SINS GPS Navigation Kalman Filter
Rotation
- 基于等效旋转矢量法的捷联惯导系统仿真，详细阐述了利用等效旋转矢量法来进行捷联惯导解算，和其实现-Rotation vector method based on the simulation of strapdown inertial navigation system in detail using the rotation vector method to calculate SINS, and its realization
SINS_Kalman
- 捷联惯性导航系统、GPS/SINS组合导航系统仿真程序-Strapdown inertial navigation systems, GPS/SINS Integrated Navigation System Simulation Program
sins
- 惯导解算，采用二子样算法，补偿了旋转误差以及划桨误差。-INS Solution
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
SINS
- SINS system jitter coupling style study
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
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-GPS-Aided--Initial-for-SINS
- 本文针对捷联惯导系统(SINS)初始对准问题,提出了一种无需经历传统的粗对准阶段而利用单天线GPS辅助直接进行动基座精确初始对准的新方法 -In this paper, SINS (SINS) initial alignment problem, we propose a coarse alignment without experiencing the traditional stages of a single-antenna GPS-assisted direct precise mo
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
CDKF-method-on-the-SINS-
- 文章基于欧拉平台误差角的概念,建立了大失准角条件下的捷联惯导系统(SINS)非线性误 差模型 -Based on the concept of Euler error angle platform, the establishment of a large misalignment angle under the conditions of SINS (SINS) non-linear error model, in practical applications more simple
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.
SINS-initial-alignment-of-several
- 捷联惯导系统初始对准几种不同滤波方法对比matlab程序-SINS initial alignment of several different filtering matlab program
Design-and-Analysis-of-GPS-SINS-Integrated-System
- A very good paper describing the detail of SINS and GPS integration