搜索资源列表
secondexalign
- 该算法用于实现静基座二位置捷联惯导初始对准-The algorithm used to implement static base two position SINS initial alignment
kfstatic
- 静基座下的SINS初始对准kalman滤波程序-The static base SINS initial alignment kalman filtering procedures
SINSmatalb
- 捷联惯导SINS静态仿真 matalb 关于四元数法捷联惯导解算算法的matlab程序组合包，其中包括滤波初始对准仿真，罗经法初始对准仿真，捷联惯导解算仿真，组合卡尔曼滤波等演示程序及其必需的参数矩阵转换程序.-SINS SINS static simulation matalb on quaternion SINS algorithm matlab program solver combination package that includes filtering the initial
Simplified-UKF-
- 简化UKF滤波在SINS大失准角初始对准中的应用-Simplified UKF filter in SINS initial alignment for large misalignment angle of
postdoctor-research-report
- 严恭敏博士后研究工作报告——捷联惯导系统动基座初始对准及其它相关问题研究报告 内容包括：大失准角下捷联惯导系统动基座初始对准，激光陀螺整周期采样对姿态解算的影响极其修正方法。SINS内杆臂效应分析与补偿，圆锥误差补偿。-Yan Gong Min postdoctoral research report- Moving Base SINS initial alignment study and other related issues Content includes: Large Mis
main
- 利用参数辨识法提取相关对准参数，从而估计出陀螺漂移和数学平台偏角并进行补偿。仿真结果表明，开路罗经法对准具有较高的对准精度、较好的快速性，能够满足捷联惯导系统在静基座下实现自对准的要求。-Expressions of mathematical platform misalignment angles of the open-loop algorithm are derived and parameter identification method is used to pick-up the
test2
- 基于基础卡尔曼滤波的捷联惯导系统初始对准，精对准，静基座。-Based on SINS initial alignment-based Kalman filter, fine alignment, static base.
lowpassfilter
- 在捷联惯导初始对准中，由于偏航角的误差较大，对准速度较慢，增加了低通滤波器，并通过横滚角和俯仰角来加快对准速度-In SINS initial alignment, the error of yaw angle, aligning slower, increasing the low-pass filter, and through the roll angle and pitch angle to accelerate the speed of the alignment
kalmaninitialize
- 利用GPS和SINS组合来对捷联惯导初始对准进行仿真，效果较好-Use a combination of GPS and SINS SINS initial alignment for the simulation, better
jie
- 捷联惯导初始对准程序m 文件，主要用于惯性导航的初始对准-SINS initial alignment procedure m file，The initial alignment is mainly used for inertial navigation
Kalman_sins_alignment
- 一个捷连惯性导航系统的初始对准仿真程序，其设计依据详见《捷联惯导系统初始对准滤波技术研究》，该论文通过CK可以方便下载。-This is a simulation program of initial alignment of inertial navigation system, its design basis as described in SINS initial alignment filtering technology research , the paper can be ea
Liru_1_DynamicAlignment_Coarse
- 我们卫星定位导航课中导航中双历元GNSS辅助SINS动态初始对准方法的m文件，只要有测量数据应该就可以实现，大家可以参考一下-Our lesson navigation satellite positioning and navigation double epoch dynamic GNSS assistance SINS initial alignment method m file, as long as the measurement data should be able to ach
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.
Kalman
- 捷联惯性导航，利用卡尔曼滤波，matlab程序，关于初始对准-SINS initial alignment procedure Kalman
Kalman1
- 捷联惯性导航Kalman小失准角精对准程序-SINS Kalman small fine misalignment angle alignment procedure
Inertial-Navigation-System-program
- 严恭敏老师编写的SINS的Matlab仿真程序，包括大方位误差角扩展卡尔曼（EKF），滤波初始对准仿真，静态惯导/星敏感器组合，大姿态误差角非线性状态模型，UKF滤波。-Yan Gong Min teacher preparation SINS of Matlab simulation program, including large azimuth error extended Kalman (EKF), filtering initial alignment simulation, stat
PSINS
- 工具箱主要功能: 1） 姿态向量、四元数、矩阵、滤波算法等各类子程序 2） 圆锥运动仿真 划船运动仿真 惯性器件随机误差仿真 3） Kalman滤波初始对准 基于惯性系初始对准 罗经法初始对准 大方位失准角EKF初始对准 大失准角UKF初始对准 速度+姿态传递对准 4） 纯惯性导航SINS仿真 航位推算、SINS/DR仿真 SINS/GPS组合仿真 GPS/BD/GLONASS单点伪距定位 SINS/GPS松/紧组合
stukf
- 此程序是运用强跟踪UKF滤波实现捷联惯导实现初始对准，可以仿真数据，如果有实验数据也可以用！效果还可以。-This procedure is the use of strong tracking UKF SINS to achieve the initial alignment, simulation data, if the experimental data can be used! Effect can also be.
Kalman_Ultasonic_Constant.m
- alignment for SINS on stationary base Kalman filtering
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)