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利用卡尔曼滤波算法估计惯导系统状态量的源代码~谢谢分享-Source code using the Kalman filter algorithm to estimate the state variables of the Inertial Navigation System ~ Thank you to share
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把无迹卡尔曼滤波应用在惯性导航系统的处理中~用于估计状态变量误差~-Unscented Kalman filter applications in the treatment of the inertial navigation system- used to estimate the state variable error ~~
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捷联惯性导航系统中，利用四元数法进行状态变量估计~并运用到SINS/GPS组合导航系统中~-Strapdown inertial navigation system, using the quaternion method the state variables estimated ~ and applied to the SINS/GPS Integrated Navigation System ~
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Inertial Navigation System-The report documents the development of algorithms
for an inertial navigation system (INS). In general,
inertial navigation consists of three parts: Alignment,
navigation and aiding. Algorithms for these parts are
d
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上传一个word档的联邦式扩展卡尔曼粒子滤波算法，大家学习粒子滤波有益，为了使联邦滤波器够有效处理非高斯、非线性系统的状态估计问题，提出将扩展卡尔曼粒子滤波引入联邦滤波结构中，得到一种新的联邦式扩展卡尔曼粒子滤波算法.使用扩展卡尔曼粒子滤波对联邦滤波子系统的多源数据进行处理，从而摆脱了经典卡尔曼滤波的限制，拓宽了联邦滤波器的实际应用范围.将联邦式扩展卡尔曼粒子滤波算法应用于非线性滤波器的一个标准验证模型进行了仿真实验，结果表明该算法是有效性的.-Abstract: A new particle
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直接利用两水平失准角快速收敛的估计结果对传统多位里对准中方位失准角的估计，提高了捷联惯导系统静基座对准的精度和速度。-Two level losing accuracy angle rapid convergence directly the estimate result to traditional many to the position losing accuracy angle estimate, thus increased the precision which and the s
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惯导工具箱，组合导航，用于导航方面，非常好的源代码-Inertial navigation toolbox, integrated navigation for navigation, a very good source code
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惯性导航的解算实现，是一个论文。代码比较简洁，容易懂-The inertial navigation solver achieved a thesis. The code is simple, easy to understand! !
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airborne inertial-SLAM 是目前无人机在未知环境中实现导航的重要手段。-airborne inertial-SLAM is very important for UAV navigation in unknown environment.
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产生陀螺和加速度计的数据，以便在组合导航或者纯惯性导航中进行仿真-A gyroscope and accelerometer data, so the combination of navigation or pure inertial navigation simulation
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该算法利用卡尔曼滤波技术实现惯性导航与GPS组合导航-The algorithm uses the Kalman filtering technique to achieve inertial navigation and GPS Navigation
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在惯性导航系统导航结算过程中对初始姿态的初始化设定。-Initial posture in the settlement process of the inertial navigation system navigation initialization settings.
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惯性导航系统结算过程中捷联惯导算法杆臂效应算法-Inertial navigation system in the the SINS algorithm rod arm effect algorithm
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惯性导航系统中，惯导解算过程中组合导航算法-Inertial navigation systems, inertial navigation solution integrated navigation algorithm
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接连惯性导航算法中，运用卡尔曼滤波算法的方程计算-Series of inertial navigation algorithm, using the equation of the Kalman filter algorithm
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严老师编写的惯性/GPS组合导航相关程序，包括轨迹生成、滤波、解算等-Inertial/GPS navigation strict teacher written procedures, including trajectory generation, filtering solver
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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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完整惯性导航解算，能够输出惯导解算出的东北天向速度和横滚、俯仰及偏航角。-Complete inertial navigation solver, able to output the INS the solution calculated Northeast days to speed and roll, pitch and yaw angle.
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国外的一个惯性导航系统仿真工具箱，自己点滴注释过，能进行导航解算，组合导航。-An inertial navigation system simulation toolbox。 own drip comment, navigate solver integrated navigation.
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关于惯导算法的一般程序，主要针对捷联惯导-Inertial navigation algorithm general procedures for SINS
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