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1下载：
惯性导航中的粗对准程序，此算法广泛应用于精度比较低的导航测试领域。无解压密码。-Inertial Navigation rough alignment procedure, the algorithm is widely used in a relatively low accuracy navigation testing. Without extracting passwords.
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光纤陀螺仪的光学器件偏振特性测试方法研究，惯性导航与光器件方面可用-fiber optical gyroscope devices polarization characteristics testing method, inertial navigation and the available optical devices
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惯性导航算法,实现陀螺仪的仿真,用于陀螺选型-inertial navigation algorithm, and the simulation gyroscope for gyro Selection
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惯性导航捷联解算程序，坐标系采用北东地坐标-strapdown inertial navigation solution procedures, using coordinates to the coordinates of the North East
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惯性导航研究中的轨迹发生器，用于模拟载体的机动运动-inertial navigation study the trajectory generator to simulate carrier mobile campaign
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用于惯性导航的初始对准，采用北东地坐标系，10个状态量-for use in inertial navigation initial alignment using the North East to coordinate system, 10 state variables
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这是本人编写的一个接联惯性导航系统解析粗对准的仿真程序，其中分别采用了传统和改进的解析对准算法。-This is the one I prepared received Inertial Navigation System Analysis rough at the simulation program, which were used to the traditional and improved analytical alignment algorithm.
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这是一个本人编写的一个接联惯性导航系统解析粗对准程序可观测性分析的一个程序。-This is the one I prepared received an Inertial Navigation System Analysis rough alignment procedures observability analysis of a trip sequence.
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这是本人编写的接联惯性导航系统静基座对准精对准卡尔曼滤波仿真程序。请多多执教。-this is my preparation access inertial navigation system at the base of static precision alignment Kalman filter simulation program. Please excuse to teach.
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这是本人用SIMLINK辨析的一个用经典控制理论方法实现的接联惯性导航系统精对准的方法程序。-using SIMLINK Analysis with the use of a classical control theory method of access inertial navigation systems EC precision alignment methods and procedures.
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这是一个用MATLAB编写的接联惯性导航系统精对准阶段KALMAN滤波仿真程序的修正程序。解决了因系数矩阵条件数过大造成的滤波发散问题。-using MATLAB access Inertial Navigation System precision alignment stage Kalman filtering imitation really procedures amendment procedure. Solutions for the coefficient matrix sever
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关于组合导航和卡尔曼滤波的文章及程序，内容比较丰富，可以作为参考-Matlab simulation of the GPS and inertial navigation system.
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采用经典的双子样算法，实现完整的惯性导航计算。程序中还留有GPS组合导航计算的接口，供开发者进行使用。-Classic two sample algorithm to achieve complete inertial navigation calculations. The program also left interface GPS navigation calculations for developers to use.
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基本的惯性导航解算过程以及摇摆条件下的惯性导航程序-Inertial navigation program under the basic inertial navigation solution process and the swing conditions
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基于MATLAB的双子样惯导解算算法实现，可以直接调用-A mfile based on the MATLAB of the two- type inertial navigation algorithm algorithm to achieve, which can be called directly.
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捷联惯性导航中的极区位置导航，使用matlab编写，很好用。-The strapdown inertial navigation in polar position navigation, written using MATLAB, very good use.
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此程序用于激光陀螺在用于惯性导航解算，其采用双子样算法(program for inertial navigation)
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利用STM32F103作为主控，陀螺仪作为惯性传感器，可导航小车在无GPS情况下走直线，误差照成由于没增加磁陀螺的原因无法校准航向角的累积误差，所以长时间运行会带来累积误差，如果有不需要磁陀螺就可以校准的方法欢迎大家给我留言提建议。(By using STM32F103 as main control, gyroscope as inertial sensors, navigation in the car without GPS. Straight line error according t
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对惯性导航、卫星导航以及组合导航系统进行理论仿真分析(Theoretical simulation and analysis of inertial navigation, satellite navigation and integrated navigation system)
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该程序基于MATLAB平台编写，实现了GPS/INS基于位置松组合的卡拉曼滤波算法，分为两部分，GPS_INS.m为组合算法主文件，输入捷联惯导平台实测数据，设置各量测噪声参数，在调用卡尔曼滤波函数进行数据融合校正，最后实现绘图功能；kalman_GPS_INS.m 为卡拉曼滤波程序，输入量测误差以及各噪声参数可得位置和速度估计值。(The program is based on MATLAB platform, and realizes the Kalman filtering algori
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