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
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
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.
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
SINS-Alignment(C)
- 捷联惯导初始对准的C程序，包括静基座和动基座。-Initial Alignment of SINS C procedures, including stationary base and moving base.
SINS-Alignment(C)
- 捷联惯导初始对准的C程序，包括静基座和动基座。-Initial Alignment of SINS C procedures, including stationary base and moving base.
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
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,
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
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
sins-alignment
- 严恭敏的惯导系统工具箱，有初始对准的相关程序。-Yan Gong Min Inertial Navigation System Toolbox, an initial alignment procedures.
csdz
- 捷联惯导初始对准MATLAB仿真文件，应用卡尔曼滤波(SINS initial alignment MATLAB simulation files, using Calman filtering)