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SINS-MatlabImplement
- 惯性导航系统仿真算法程序，分为多个模块，编写程序时只需调用函数即可-Inertial navigation system simulation algorithm procedures, divided into multiple modules, only when the program calls the function can be
auv-navigation
- AUV惯性导航系统matlab仿真程序，包括轨迹生成、gps和sins组合、gps和dvl组合-AUV navigation system，including sins、gps、dvl and so on.
jielianguandao
- 惯性导航系统属于一种推算导航方式．即从一已知点的位置根据连续测得的运载体航向角和速度推算出其下一点的位置．因而可连续测出运动体的当前位置。惯性导航系统中的陀螺仪用来形成一个导航坐标系使加速度计的测量轴稳定在该坐标系中并给出航向和姿态角-Inertial navigation system is a dead reckoning navigation mode. That is from a given point according to the measured continuous carr
jielianguandaowuchayuan
- 惯性导航系统通常由惯性测量装置、计算机、控制显示器等组成。惯性测量装置包括加速度计和陀螺仪,又称惯性导航组合。3个自由度陀螺仪用来测量飞行器的三个转动运动；3个加速度计用来测量飞行器的3个平移运动的加速度。计算机根据测得的加速度信号计算出飞行器的速度和位置数据。控制显示器显示各种导航参数-Inertial navigation system usually means from the inertial measurement, control, computer monitor etc.. I
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
UKF-GPS-IMU_matlab
- UKF应用于GPS-IMU组合导航系统的MATLAB代码-UKF for the PS-IMU GNC system of MATLAB code
SINS-Calculation
- 惯性导航系统精解算程序 -Inertial navigation system-Inertial navigation system calculation
LSPzuhe14_8
- 多星座导航系统中利用最小二乘算法进行位置解算的MATLAB傆代码，以GPS/GLONASS系统为例-Multi-constellation navigation system using least square algorithm solver of MATLAB Yuan location code to GPS/GLONASS system as an example
GDOP_6_A
- 多星座导航系统GDOP递推特性的仿真程序-GDOP recursive multi-constellation navigation system features simulation program
GDOP_6_AB
- 多星座导航系统GDOP递推特性的仿真程序,程序主要是争对在现有系统中增加一颗现有星座的可见星时GDOP的变化情况组合仿真-GDOP recursive multi-constellation navigation system features simulation program, the program is primarily a struggle for an increase in the existing system, the existing constellation of s
GDOP_6_AC
- 多星座导航系统GDOP递推特性的仿真程序,程序主要是争对在现有系统中增加一颗现有星座的可见星，一颗其他星座的可见星时GDOP的变化情况组合仿真-GDOP recursive multi-constellation navigation system features simulation program, the program is mainly a struggle to increase the existing constellation of stars visible in the
GDOP_6_CC
- 多星座导航系统GDOP递推特性的仿真程序,程序主要是争对在现有系统中增加一颗其他星座的可见星时GDOP的变化情况组合仿真-GDOP recursive multi-constellation navigation system features simulation program, the program is mainly a fight for increases in existing systems of other constellations visible changes in
GDOP_6_BB
- 多星座导航系统GDOP递推特性的仿真程序,程序主要是争对在现有系统中增加2颗现有星座的可见星时GDOP的变化情况组合仿真-GDOP combination of changes in multi-constellation navigation system simulation GDOP recursive feature of the simulation program, the program mainly to fight for increased two existing cons
GDOP_6_CD
- 多星座导航系统GDOP递推特性的仿真程序,程序主要是争对在现有系统中增加2颗其他星座的可见星时GDOP的变化情况组合仿真-GDOP combination of changes in multi-constellation navigation system simulation GDOP recursive feature of the simulation program, the program mainly to fight for increased two existing cons
dual_2
- 惯性导航系统误差仿真，针对捷联惯导系统的误差方程进行仿真，得到误差曲线-error simulation
matlab-toolbox-forINS
- 惯性导航系统的matlab工具箱，里面包含使用说明以及各个m文件的功能-Inertial navigation system matlab toolbox, which contains instructions for use and various m-file function
chunguanxing
- 惯性导航，利用惯性元件（加速度计）来测量运载体本身的加速度，经过积分和运算得到速度和位置，从而达到对运载体导航定位的目的。组成惯性导航系统的设备都安装在运载体内，工作时不依赖外界信息，也不向外界辐射能量，不易受到干扰，是一种自主式导航系统。-Inertial navigation, to measure the carrier itself acceleration Inertial element (accelerometer), through integration and operati
cuduizhun
- 惯性导航系统开始导航之前的工作状态。在此期间，一般进行坐标系对准、初始参数的测定和装定。-Inertial navigation system before starting work state navigation. In the meantime, the general alignment of the coordinate system, initial parameters measured and setter.
Matlab-INS-toolbox
- 该惯性导航系统工具箱（INS）就是专门为这个目的设计的。这个工具箱可以用来模拟仿真载体动力学，处理原始测量值（加速计上的delta-V数据和陀螺仪上的delte-theta数据）和数据。-The inertial navigation system (INS) is specially designed for this purpose. The kit can be used to simulate carrier dynamics, processing raw measurements (
ajtyzjgn
- 几个BOC 信号的分析例程，全球卫星导航系统将普遍采用BOC调制信号作为扩频测距信号，qByWsxD信号自相关函数呈现多个相关峰-Several of the BOC Signals analysis routines, global navigation