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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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这个是关于GPS和捷联惯性导航系统的组合导航技术研究论文,非常有参考价值.,This is about GPS and strapdown inertial navigation system, a combination of navigation technology research papers, a very good reference material.
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基于matlab平台编写的捷联导航程序，采用四元数法求解导航参数,Prepared based on matlab platform inertial navigation procedures, the use of quaternion navigation method parameter
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捷联惯性导航解算程序，内附实测数据与说明文档,Strapdown inertial navigation solution counting procedures, and inserting the measured data and documentation
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捷联惯性导航的仿真程序用四元数法的捷联惯性导航姿态解算程序资源大小:...用四元数法进行姿态解算的matlab程序,Strapdown inertial navigation simulation program
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捷联惯性导航源程序，希望对您有所帮助。谢谢大家,Strapdown inertial navigation source
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F16飞行控制仿真程序，主要是利用matlab/simulic对F16建模并对其飞行条件进行仿真-Strapdown inertial navigation static base and the platform initial alignment process, C language, a good routine
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捷联导航相关知识，陀螺，及速度及惯性敏感器件和测试、补偿标定技术以及捷联系统算法的相关知识-Strapdown navigation knowledge, gyro, and speed and inertia-sensitive devices and tests, calibration and compensation algorithms SINS knowledge
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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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捷联与平台惯导静基座初始对准程序,C语言编写，很好的例程-Strapdown inertial navigation static base and the platform initial alignment process, C language, a good routine
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一、数据说明：
1：惯导系统为指北方位的捷连系统。初始经度为116.344695283度、纬度为39.975172度,高度h为30米。
初速度为v0=[0.000048637 0.000206947 0.007106781]，飞行高度不变。
2：jlfw中为600秒的数据，陀螺仪和加速度计采样周期分别为为1/80秒和1/80秒。
3：初始姿态角为[0.120992605 0.010445947 91.637207]（俯仰，横滚，航向,单位为度）,
jlfw中保存的为比力信
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捷联惯导系统导航解算.
根据600秒的指北方位捷联系统的数据进行导航解算，飞行高度不变，采样周期0.01s.-Strapdown inertial navigation system navigation solution. Based on the 600 seconds that the north-bit data SINS navigation solution, the same altitude, sampling period 0.01s.
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这是低精度光纤捷联惯导与GPS组合的博士论文,内容丰富,希望对需要的人有用!-This is a low-accuracy fiber-optic strapdown inertial navigation and GPS combination of doctoral dissertation, rich in content, in the hope that those who need it useful!
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基于Matlab平台开发的的针对捷联式惯性到导航的仿真，比较全的代码-Matlab-based platform for the development of strapdown inertial navigation simulation to compare the entire code
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利用matlab数值计算的强大功能和,建模容易实现的特点"进行了捷联式惯性导航系统的仿真研究,对四元数及姿态矩阵等的解算采用编程实现"陀螺仪和加速计的建模用.-Matlab numerical calculation using the power and, modeling the characteristics of easy to implement " a strapdown inertial navigation system of the simulation study a
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基于MATLAB Simul ink 的捷联惯性导航系统仿真,主要介绍了其基本原理，然后阐述了编程实现-MATLAB Simul ink based on the strapdown inertial navigation system simulation, introduces the basic principles of programming and then set out to achieve
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《Strapdown inertial navigation technology》全面系统地介绍了捷联惯导的基本原理与计算。-Strapdown inertial navigation technology， a comprehensive and systematic introduction to the basic principles of strapdown inertial navigation system and calculation.
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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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Matlab code for Strapdown navigation system alignment-Matlab code for Strapdown navigation system alignment.
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捷联惯性导航技术,经典电子书
Strapdown navigation technology
中文版-Inertial navigation technology, the classic book Strapdown Inertial Navigation Technology David H. Titterton Jobn L. Weston Chinese
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