搜索资源列表
CNS
- 天文导航，弹道导弹SINS/CNS组合导航，轨迹发生器，卡尔曼滤波-Celestial navigation, ballistic missile SINS/CNS integrated navigation, trajectory generator, Kalman filtering
GPS_SINS
- 捷联惯导系统的导航算法，采用卡尔曼滤波对惯性信息和GPS信号进行融合，进行噪声处理-SINS navigation algorithm, Kalman filtering fusion of inertial information and GPS signal, noise processing
newSINS
- 关于惯导算法的一般程序，主要针对捷联惯导-Inertial navigation algorithm general procedures for SINS
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
denoise1
- 编写的小波去噪程序，主要用于光纤捷联惯导系统中的惯性器件输出噪声滤除，为后续导航解算提供基础-The wavelet denoising program written mainly used in fiber SINS the inertial device output noise filtering, to provide a basis for subsequent navigation solution
sins
- 捷连惯性导航,这是关于现在兴起的导航，采用仿真的形式-Jielian inertial navigation, which is now the rise of the navigation, the use of simulation in the form of
DGP-SINS-Integrated-Pos
- 武汉大学的一篇关于INS/GPS组合导航的论文，非常经典，算法和实验结果都非常详细！用中国知网阅读器打开-Wuhan University, very classic article on the papers of the INS/GPS integrated navigation algorithms and experimental results are very detailed! Chinese HowNet reader opens
RungKutta
- GPS/捷联惯导组合导航中的龙格库塔法的解算，在matlab程序中使用-Runge-Kutta method for solving GPS/SINS integrated navigation, matlab program
INS-and-dead-reckoning-combination
- 捷联惯导与行位推算，构成组合导航系统，INS和航位推算组合-The SINS line reckoning that constitute the integrated navigation system, INS, and the combination of dead reckoning
Initial-alignment
- 捷联惯导初始对准程序，主惯导与子惯导初始对准-SINS initial alignment procedure, the main INS and sub-inertial alignment
my_sins
- 本程序实现SINS捷联解算，提供给惯性期间信息即可得到导航参数-The program SINS Jie associated solver, information provided to the inertia during navigation parameters can be obtained
longku_4
- 捷联惯导中用于计算四元数微分方程的四阶龙格库塔法matlab程序-SINS quaternion differential equations used to calculate the fourth-order Runge-Kutta method matlab program
strapdown
- matlab实现捷联惯性导航解算，四元数更新姿态矩阵。-SINS solver matlab
INS
- 捷联惯导的解算程序，大家一起学习交流，有疑问的可以联系我。-The calculating program of sins, we learn together.
trajectory-simulation
- 用于做GPS/SINS、或SINS导航时要用到的初始数据发生程序-For the initial data of GPS\/SINS, or SINS navigation to be used
kalman_linear_gai
- 卡尔曼滤波程序，系统为捷联惯导，维数为15的系统方程，参考书目是秦永元惯性导航-Kalman filtering process, the system for the sins, the dimension of the system of 15 equations, a bibliography is ROCKETS inertial navigation
ins
- 捷联惯导结算程序，读取数据文件，东北天地理坐标系，最后给出位置速度和姿态-SINS settlement procedures, read data files, Northeast days geographic coordinate system, and finally gives position, velocity and attitude
SINS
- 惯性导航解算程序，四阶龙格库塔发更新四元数，求姿态，解算位置速度-Inertial navigation solver
sins
- 捷联惯导原理及程序，简要介绍捷联惯导方程，并附程序-strapdown inertial navigation
ukf-ands-_ukf
- ukf sukf and ekf for GPS/SINS application -ukf ekf sukf