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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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惯性导航+GPS组合导航，经典算法，不要错过。-Inertial Navigation+ GPS navigation, the classical algorithm, do not miss.
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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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MATLAB惯性导航工具箱，有详细的中文说明和例程，适合初学者使用。-Inertial navigation MATLAB toolbox, detailed descr iptions and routines of Chinese for beginners.
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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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Global Positioning Systems Inertial Navigation And Integratio
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利用比力、加速度信息解算出惯性导航所需的速度、位置和姿态信息-Than the use of force, acceleration of information required for inertial navigation solution to calculate the speed, position and attitude information
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惯性导航系统仿真试验研究及其详细的编程实现方法-Inertial navigation system and its simulation programming
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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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在MATLAB环境下，使用GPS与惯性导航技术相结合的联合导航卡尔曼滤波算法-In the MATLAB environment, the use of GPS and inertial navigation technology joint navigation Kalman filter algorithm
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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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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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通过卡尔曼滤波并采用开环控制方式实现惯性导航和GPS的数据融合-Through the Kalman filter and use the open-loop control method to achieve inertial navigation and GPS, data fusion
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利用静基座下惯性导航系统的误差方程，用matlab/simulink建立了惯导误差仿真模型-The use of static base under the inertial navigation system error equation, using matlab/simulink simulation model established the INS error
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GPS与惯性导航系统组成的组合导航系统仿真程序-GPS and inertial navigation system consisting of integrated navigation system simulation program
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MatLab Files for
GLOBAL
POSITIONING SYSTEMS,
INERTIAL NAVIGATION,
AND INTEGRATION
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GPS惯性导航MATLAB工具箱-MATLAB源代码，适合于惯性导航的初学者研究，有利于初学者掌握INS/GPS组合导航-GPS inertial navigation MATLAB toolbox of MATLAB source code, suitable for inertial navigation beginners, beginners to master the INS / GPS Integrated Navigation
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inertial navigation algorithm matlab program, a routine
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惯性导航的解算，附带速度、姿态、位置的姿态解算，内容很全(Inertial navigation solution, with speed, attitude, position of the attitude calculation, the content is very complete)
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