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捷联惯性导航技术中使用四元数算法实现姿态更新矩阵的求解，得到姿态角。-Strapdown inertial navigation technology using quaternion attitude update algorithm for solving the matrix, get attitude angle.
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微型惯性测量组合(MIMU：Micro-inertial measurement unit)是国际上近年来发展起来的新技
术，作为一种不依赖任何外部信息，也不向外部辐射能量的自主式系统-Abstract：The Micro strapdown inertial measurement unit
System are introduced, attitude algorithm and Kalman
filtering equation of parameter identifying
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最近在弄陀螺稳定，得到这篇很经典的资料，江南航天集团的。捷联式惯性导航积分算法。很稀罕的。-Get gyro stabilized recently received information of this classic, Jiangnan Aerospace Group. Strapdown inertial navigation integration algorithm. Very rare for.
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捷联惯性导航与GPS组合导航。采用matlab实现。采用自适应算法对其进行处理。并取得了很好的效果。-Strapdown inertial navigation and GPS Navigation. Using matlab to achieve. Adaptive algorithm used to deal with them. And has achieved good results.
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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.
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捷联算法的公用函数，是进行捷联航姿算法的必备的公用函数也是组合导航的公用函数-Strapdown algorithm common function is to carry out AHRS algorithms essential public functions are common functions Navigation
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捷联算法，与公共函数结合一起，构成完整的捷联算法。-Strapdown algorithm, combined with public functions together with a complete strapdown algorithm.
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捷联惯性导航滤波算法ｍａｔｌａｂ仿真,一定对哪些初学者有帮助-strapdown navigationg filtering algorithm
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程序用仿真的方法编制了捷联惯导系统的姿态和航向角解算算法，适合学习算法用。-it is a good programme for them who is studying the algorithm of strapdown inertial navigation.
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基于圆锥误差补偿算法和划船误差补偿算法的等效原理，可将圆锥误差补偿算法移植到划船误差补偿对圆锥误差补偿算法和捷联惯导算法进行了仿真。给出了Matlab的m文件源程序代码具有一定的参考价值。
-Based on the coning error compensation algorithm and the sculling error compensation algorithm of equivalent principle, the coning error compensation al
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指北方位系统在捷联惯性导航系统中的matlab模拟算法-Matlab simulation algorithm north-bit system in strapdown inertial navigation system
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最近在弄陀螺稳定，得到这篇很经典的资料，江南航天集团的。。捷联式惯性导航积分算法。很稀罕的。，已通过测试。
-Recently worked on the gyro-stabilized, this classic data, Jiangnan Space Group. . Strapdown inertial navigation integration algorithm. Very rare. , Has been tested.
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捷联惯性导航的算法，去掉两个个参数后的改进算法可直接使用。
-Strapdown inertial navigation algorithm, remove the two parameters of the improved algorithm can be used directly.
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捷联惯导系统仿真数据生成工具，，可以用来验证捷联算法可直接使用。
-SINS simulation data generation tool that can be used to verify that the strapdown algorithm can be used directly.
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一个简单的捷联姿态解算算法 GPS-INS惯导算法-A simple strapdown attitude solver algorithm GPS-INS inertial navigation algorithm
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基于Matlab_的捷联惯导算法设计及仿真.pdf-Based on the Matlab strapdown inertial navigation algorithm design and simulation
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LM算法的MATLAB实现。Levenberg-Marquardt算法是最优化算法中的一种。最优化是寻找使得函数值最小的参数向量。-LM algorithm in MATLAB. Levenberg-Marquardt algorithm is an optimization algorithm. Optimization is to find the minimum value makes the function parameter vector.
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运用四元数方法进行捷联惯性系统的姿态解算，并由加速度计的数据和陀螺的数据计算导航参数-The four element method for strapdown inertial navigation system of the attitude calculation, and the accelerometer and gyroscope data data computation of navigation parameters
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捷联惯性导航姿态解算原理及核心算法,从原理到最终程序实现-Strapdown inertial navigation attitude algorithm principle and the core algorithm, the principle to the final program
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捷联惯导程序，依据加表和陀螺仪的输出数据来求解飞行器的姿态-Strapdown inertial navigation algorithm matlab
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