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guijishuju
- 捷联惯性导航的姿态数据自动生成，利用C程序实现，可用于验证接连导航程序。-Posture of strapdown inertial navigation data automatically generated using the C program implementation, can be used to verify the series of navigation program.
kem
- 卡尔曼滤波算法在飞行器中的应用。根据惯性导航原理，采用卡尔曼滤波，对飞行器的横滚角、俯昂角进行校准。达到预期效果。-Kalman filtering algorithm in aircraft application. According to principles of inertial navigation, Kalman filtering, the aircraft' s roll angle, overlooking the Ngong angle calibration. To
GPS-INSmatlab
- 关于GPS/INS组合导航的matlab仿真程序 大家共同学习下-On GPS/INS Integrated Navigation System of the matlab simulation program to study under the common
strapdown
- 惯性导航捷联算法的matlab实现，内附举例坐标点。-Strapdown inertial navigation algorithm matlab implementation, enclosing the coordinates of points, for example.
RtwMatrix
- GPS惯性导航系统,解压后会有5M,这是我利用C#针对嵌入式WinCE做的一个GPS/惯性导航系统的组合定位软件，包括了卡尔曼滤波算法（含矩阵控件），界面显示，GPS串口接受，滤波结果输出以及WinCE应用调试控件，超强吧！直接下载可以在Visual.Net下调试使用-GPS inertial navigation system, after decompression will be 5M, which I use C# for embedded WinCE do a GPS/inertial
jwg_li_co
- 此程序功能为输入发射点重力惯性坐标系下的坐标，求出当时的地理经、纬、高；-This program functions as the input launch point gravity inertial coordinate system of coordinates, then find the geographic, economic, weft, high
Kepler_orbit_rotate
- 计算得出导弹的被动段飞行轨迹（未考虑大气）和再入点、落点信息（在发射惯性坐标系内的位置量）-Calculated the passive missile flight path segment (not to consider the atmosphere) and re-entry point, placement of information (in the firing position within the inertial coordinate system volume)
trans_p
- 此程序是实现由发射惯性坐标系到地理经纬度的转换-This program is to achieve by the launch of inertial coordinates to geographic latitude and longitude conversion
Introduction_to_Inertial_Navigation
- Introduction to Inertial Navigation
bi_device
- Driver written on Qt version 4.6.0 for gimballess inertial device
Integratedgps
- Integrated Inertial, GPS, and LORAN System，国外的一个多媒体，介绍的比较不错-Integrated Inertial, GPS, and LORAN System, a multimedia abroad, presented a good comparison
kaerman
- 卡尔曼滤波器，用于平滑惯性器件的输出数据，从而可以对数据进行建模与补偿。 -Kalman filter, inertial device for smoothing the output data, allowing for data modeling and compensation.
CHAP7_1
- 被控对象为两惯性模型，调节器为PI调节器并在系统中加入了整数阶干扰观测器-Inertial model for the two charged objects, regulator for the PI regulator and in the system by adding the integer-order disturbance observer
untitledlly3
- 加入二项式滤波器的干扰观测器系统。被控对象为两惯性模型，调节器为传统PID控制器- the binomial system of disturbance observer filter. Inertial model for the two charged objects, the traditional PID controller regulator
navigation
- 一本很不错的关于惯性导航的书籍，对惯性基本方程以及算法编程，都有很好的说明。-A very good book on the inertial navigation, the basic equation of the inertia and the algorithm programming, have a good explanation.
123
- 惯性导航工具箱，可以实现多种仿真。感兴趣的-Inertial navigation toolbox, can achieve various simulation. Interested to see
naoqu_w_slave_maste
- 根据主子惯性导航系统角速率之差计算 挠曲 该代码只是个计算的例子,提供方法.传递对准中的挠曲和柑臂计算,-Master inertial navigation system based on the difference between the calculated deflection angle rate is just a calculation of the code examples provide a way. Transfer alignment and orange arm de
ballistic_missile_inertial_navigation
- 弹道导弹从东经120北纬20高度30公里打目标东经150北纬30高度0的目标，关机点及飞行时间计算。还介绍了惯性导航的内容。 对于弹道式导弹：目标作为地球上的某一点，它是随地球一起在惯性空间运动的，因此需要迭代求解需要速度和自由飞行时间。按照给出的程序进行多次迭代解算即可得出考虑地球自转时的关机点参数解算和飞行时间计算。-20 ballistic missile from a high degree of north latitude and 120 east longitude hit tar
insjiesuan
- 惯性导航的Matlab程序，可以直接运行-Inertial navigation of Matlab procedures, can be directly run-Inertial navigation Matlab program, you can directly run-Inertial navigation of Matlab procedures, can be directly run
gpsinertial
- gps+inertial using C# gps惯性导航-gps+inertial using C#