搜索资源列表
INS
- 惯性导航系统仿真用来描述导航系统的导航方法，最后做出一系列的仿真图形来判断导航的效果。-Inertial navigation system is a common kind of navigation system.It is widely used in a lot of fields including military and civil applications.
INS_OUT
- 惯性导航的分针分析，可以模拟出不同观测角，不同方向的速度-The minute hand of the inertial navigation analysis, we can simulate different viewing angle, the speed of different directions
Navigation_3_1
- 惯性导航的姿态解算，四元数解算，导航定位解算等-Inertial navigation attitude algorithm, the Quaternion solution, such as navigation and position
SINS-VelAlignment-time-delay-MATLAB
- 关于捷联惯性导航传递对准的仿真程序，期待学术交流~谢谢分享~-Simulation program on Transfer Alignment of Strapdown Inertial Navigation and look forward to the academic exchange ~ Thank you for sharing ~
INS-alignment
- 关于惯性导航系统传递对准与系统参数误差分析的源代码~谢谢分享-Share on the passing of the inertial navigation system alignment and error analysis of the source code ~ Thank you
UPF
- 把无迹卡尔曼滤波应用在惯性导航系统的处理中~用于估计状态变量误差~-Unscented Kalman filter applications in the treatment of the inertial navigation system- used to estimate the state variable error ~~
SINS
- 捷联惯性导航系统中，利用四元数法进行状态变量估计~并运用到SINS/GPS组合导航系统中~-Strapdown inertial navigation system, using the quaternion method the state variables estimated ~ and applied to the SINS/GPS Integrated Navigation System ~
Paul_G.Savage
- GNSS接收机惯性导航处理算法技术文档,用于提高导航接收机性能，在高动态环境下具有良好的稳健性-technique paper for GNSS receiver inertial navigation algorithm
Untitled1
- 产生陀螺和加速度计的数据，以便在组合导航或者纯惯性导航中进行仿真-A gyroscope and accelerometer data, so the combination of navigation or pure inertial navigation simulation
kalman3
- 该算法利用卡尔曼滤波技术实现惯性导航与GPS组合导航-The algorithm uses the Kalman filtering technique to achieve inertial navigation and GPS Navigation
INS_Simulation
- 完整惯性导航解算，能够输出惯导解算出的东北天向速度和横滚、俯仰及偏航角。-Complete inertial navigation solver, able to output the INS the solution calculated Northeast days to speed and roll, pitch and yaw angle.
INS_ToolBox
- 国外的一个惯性导航系统仿真工具箱，自己点滴注释过，能进行导航解算，组合导航。-An inertial navigation system simulation toolbox。 own drip comment, navigate solver integrated navigation.
subfunctions
- 这个是惯性导航初始对准以及导航解算中常用的子程序-This is the inertial navigation initial alignment and navigation solver subroutine
GPS_INS
- 全球定位系统和惯性导航系统的组合导航程序，里面还有仿真的图形，很全面。-Integrated navigation program GPS and inertial navigation system, there are simulation graphics, very comprehensive.
INS-tool
- 惯性导航的工具箱，对IMU的导航计算利用Matlab进行了全面的仿真，非常适合IMU导航算法、组合导航算法的研究-Inertial navigation toolbox IMU navigation calculation using Matlab comprehensive simulation, very suitable for the IMU navigation algorithm, integrated navigation algorithm
SINS1
- 这是秦永元所著的《惯性导航》一书，根据其中的内容用matlab中的simulink编写的关于惯导基本原理的小程序，适合初学者学习，修改加以应用-the Inertial Navigation of simulink
ins1
- 北京航空航天大学《惯性导航原理》第一次大作业源程序-Beijing University of Aeronautics and Astronautics inertial navigation principle " first great source operations
ins2
- 北京航空航天大学《惯性导航原理》第二次大作业源程序-Beijing University of Aeronautics and Astronautics " principle of inertial navigation" second source operations
INS_Initialization
- 惯导系统初始对准的Matlab源代码，对于惯性导航系统的初始对准算法研究有帮助-INS initial alignment of the Matlab source code for inertial navigation system to help the initial alignment algorithm
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