搜索资源列表
JIELIAN
- 初始对准的c算法源码,实现捷联惯导的静基座初始对准-c initial alignment algorithm source code, achieving SINS the static base initial alignment
52002
- 硕士学位论文捷联惯性系统初始对准研究 惯导系统的初始对准是影响系统使用性能的关键技术之一，对准的精度与速度直接关系到惯性统的精度与启动特性。对卡尔曼滤波及其在初始对准中的应用进行了研究。首先介绍了卡尔曼滤波理论的应用背景，然后推导了离散卡尔曼滤波方程，并对连续系统的状态方程进行离散化提出了适用于舰载捷联惯性系统的动基座对准的2通道10个状态变量和2通道12个状态变量的系统动态模型，并建了相应的速度匹配和位置匹配量测模型。 -master's degree thesis SINS
zuhedaohang
- 捷联惯导和GPS组合导航程序，包含初始对准和滤波算法-SINS and GPS navigation program, including the initial alignment and filtering algorithms
mti_calibrated
- 一个非常全面的捷联惯导程序，包含了从初始对准、初值的设定，四元素的四阶龙格库塔法更新，对速度微分方程和位置方程分别用龙格库塔法和欧拉角法求解-A very comprehensive program SINS, including from the initial alignment, initial set, the four elements of the fourth order Runge-Kutta method updates the location of the speed di
InitialAliagment
- 这是几篇有关捷联惯导初始对准的期刊论文,有粒子滤波和自适应滤波,内容丰富-This is surprisingly few articles about the SINS initial alignment of journal articles, with particle filter and adaptive filtering, content-rich
chushiduizhuncanshubianhua
- 捷联惯性导航的算法，去掉两个参数后的改进算法- The initial alignment of SINS
EKFsins
- 捷联惯性导航系统的卡尔曼滤波对准程序，非常有用-alignment sins
KF
- 建立了捷联管道系统初始对准的误差模型和卡尔曼滤波模型观测方程，进行了卡尔曼滤波仿真。-The error function for initial alignment of SINS and the observation equation of Kalman filter model is built．Simulation of Kalman filter presented．
matlab
- 捷联惯性导航的卡尔曼滤波 初始对准程序-SINS initial alignment procedure of Kalman filtering
wc
- 分析初始对准误差，随机误差对捷联惯导精度的影响-Analysis of initial alignment errors, random errors on the precision of SINS
Kalman
- 捷联惯导初始对准Kalman滤程序，非常难得的代码源程序。-SINS initial alignment Kalman filter program, source code is very rare.
www_dssz_com_matlab-kf_sins
- 捷联惯导初始对准的MATLAB程序,很好用的.-SINS initial alignment of MATLAB procedures, very good use.
23
- 捷联惯导系统静基座初始对准精度分析及仿真-The SINS static base initial alignment accuracy analysis and simulation
qk_AG
- 捷联惯导卡尔曼滤波算法初始对准，参考哈工程的硕士写的，效果可以，但是不知道观测量是如何构造的。-Kalman filter algorithm SINS initial alignment, Master of Engineering Reference Kazakhstan write, the effect can be observables but do not know how to construct.
GNSS-SINS-initial-alignment-method-
- 双历元GNSS辅助SINS动态初始对准方法，获得初始时刻的位置、速度、姿态等的信息。含有初始对准程序以及测试程序，四元数计算程序-Dual Dynamic epoch GNSS assistance SINS initial alignment method to obtain the initial time position, velocity, attitude and other information. Containing the initial alignment procedur
sins
- 惯导仿真部分模块化，标准化，分为IMU模块，初始对准模块，SINS解算模块，SINS性能评价模块，SINS解算的输出为地理坐标系内速度、经纬高、姿态角,运行INS_perforEva.m可以得到惯导仿真结果。-INS simulation part modular, standardized, divided IMU module, the initial alignment module, SINS solver module, SINS performance uation module,
strapdown_kem
- 在导航应用上捷联惯导时对准中的卡尔曼滤波算法程序，是方差最小，无偏性的，实用性很强的估计算法-In the navigation application when SINS Alignment Kalman filter procedure is the minimum variance, unbiased, and very practical estimation algorithm
SINS
- 捷联惯导初始对准的C源码 -SINS initial alignment of the C source, including
76228543imu_ahrs
- SINS仿真程序，包含对准解算和组合导航模块，亲测可用(Foreign SINS simulation program, including alignment, calculation and integrated navigation module)
新建文件夹
- 通过误差分析对三种捷联惯导系 统解析粗对准方法进行了 比 较(Through the error analysis, the analytic coarse alignment methods of three sins are compared)