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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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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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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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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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基于等效旋转矢量法的捷联惯导系统仿真，详细阐述了利用等效旋转矢量法来进行捷联惯导解算，和其实现-Rotation vector method based on the simulation of strapdown inertial navigation system in detail using the rotation vector method to calculate SINS, and its realization
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Sistems inertial control Alg. Strapdown inertial navigation system
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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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捷联惯性导航系统、GPS/SINS组合导航系统仿真程序-Strapdown inertial navigation systems, GPS/SINS Integrated Navigation System Simulation Program
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基于四元数法的捷联惯性导航系统姿态解算及正弦输入函数的生成-Quaternion-based strapdown inertial navigation system attitude solution and the generation of sinusoidal input function
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MATLAB_Simulink的捷联惯性导航系统仿真-MATLAB_Simulink of strapdown inertial navigation system simulation
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对捷联惯导的速度、经纬度、姿态角等参数进行解算-A programme to compute the speed,latitude,longitude and attitude of strapdown inertial navigation system
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捷联惯性导航系统滤波程序，matlab源代码-Strapdown inertial navigation system, filtering procedures, Matlab source code
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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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捷联惯性导航系统中纯捷联的程序C语言写的-Strapdown inertial navigation system, pure strapdown program written in C language
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捷联惯性导航系统多位置对准程序卡尔曼滤波-Strapdown inertial navigation system position alignment procedure Kalman filter
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研究生讲的PPT关于捷联惯性导航系统对准的-Graduate speak PPT on the alignment of the strapdown inertial navigation system
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一段关于捷联惯导系统与GPS导航系统的Matlab仿真程序，-Matlab simulation program period of Strapdown Inertial Navigation System with GPS navigation system,
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捷联惯性导航算法完整版（单子样姿态解算算法）-Strapdown inertial system
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