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这是本人编写的一个接联惯性导航系统解析粗对准的仿真程序,其中分别采用了传统和改进的解析对准算法。-This is the one I prepared received Inertial Navigation System Analysis rough at the simulation program, which were used to the traditional and improved analytical alignment algorithm.
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这是一个本人编写的一个接联惯性导航系统解析粗对准程序可观测性分析的一个程序。-This is the one I prepared received an Inertial Navigation System Analysis rough alignment procedures observability analysis of a trip sequence.
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这是本人编写的接联惯性导航系统静基座对准精对准卡尔曼滤波仿真程序。请多多执教。-this is my preparation access inertial navigation system at the base of static precision alignment Kalman filter simulation program. Please excuse to teach.
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这是一个用MATLAB编写的接联惯性导航系统精对准阶段KALMAN滤波仿真程序的修正程序。解决了因系数矩阵条件数过大造成的滤波发散问题。-using MATLAB access Inertial Navigation System precision alignment stage Kalman filtering imitation really procedures amendment procedure. Solutions for the coefficient matrix sever
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实现了车辆惯性导航系统的卡尔曼滤波,包括定位结算,姿态校正,速度校正等,也包括惯性导航系统的模型建立,结算,白噪声,等等,对研究导航很有参考价值 -realized the vehicles inertial navigation system Kalman filtering, including clearing positioning, posture correction, the speed correction, including inertial navigation syste
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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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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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惯性导航系统传递对准系统模型程序,请大侠诚恳指教,多谢-Inertial navigation system alignment system model transfer process, please sincerely advice heroes, I would like to thank
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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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inertial navigation system developed for low cost mems sensors
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用Matlab实现对惯性导航系统(陀螺仪和加速度计)的误差分析。-Matlab to inertial navigation system (gyroscopes and accelerometers) error analysis.
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Integration of Global Positioning System and Inertial Navigation System
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Integration of Inertial Navigation System and Global Positioning System Using Kalman Filtering
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Aircraft inertial navigation control system design and simulation platform implementations
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组合导航系统介绍以MEMS技术为基础的组合导航系统,主要是惯性导航系统与卫星定位系统相结合。-Integrated navigation system is based on MEMS technology.Its main integration is inertial navigation system and global positioning system.
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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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随着GPS性能的不断完善,应用越来越广泛,但GPS系统易受到外界环境影响,而传统的惯导系统也具有误差随时间积累的缺陷,因此GPS/INS组合方式因其互补性强已经成为实现导航的重要方式。这种组合方式能够确保在采用较廉价的惯性设备的情况下,也能获得较好的导航效果。-With the constant improvement of the GPS performance, more and more widely, but the GPS system vulnerable to external e
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惯性导航系统误差传播特性分析,北航惯性导航基础大作业,内含matlab程序代码-Inertial navigation system error propagation characteristics analysis, Northern Inertial Navigation foundation work, containing matlab code
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关于组合导航和卡尔曼滤波的文章及程序,内容比较丰富,可以作为参考-Matlab simulation of the GPS and inertial navigation system.
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利用因子图和积算法设计的无人机惯性导航系统算法,利用matlab仿真实现(An algorithm of unmanned aerial vehicle (UAV) inertial navigation system designed by factor diagram and calculation method is realized by MATLAB simulation)
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