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一个实现了GPS和INS组合导航系统的程序,能够直接运行,对于研究惯导算法、组合系统算法的有一定帮助。-A realization of GPS and INS navigation system procedures can be run directly, for the study of inertial navigation algorithm, the algorithm combined system will definitely help.
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一个在导航界大牛写的一个报告,值得大家,特别是惯性导航的人员下载-A large cattle in the navigation industry to write a report, it is worth, especially inertial navigation officer download
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本程序的功能是:实现惯性导航参数的自标定过程。-Realize the self-calibration process of inertial navigation
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惯性导航解算程序,四阶龙格库塔发更新四元数,求姿态、速度和位置-Solver inertial navigation procedures, fourth-order Runge-Kutta issued to update the quaternion, seeking attitude, velocity and position
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惯性导航算法,有输入数据,在MATLAB下的哦,直接就可以运行得通,惯性技术作业哦!-Inertial navigation algorithm, the input data in MATLAB Oh, it can be shipped directly works, inertial technology jobs oh!
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一个利用无迹卡尔曼滤波进行的惯导结算程序,可以有效的减少由于线性化带来的误差-An unscented Kalman filter for use in inertial navigation settlement procedures, can effectively reduce the error caused due linearization
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惯导轨迹仿真,对于初学惯导的人有很大的帮助-INS trajectory simulation, inertial navigation for beginners who have a lot of help
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GPS惯性导航组合(第2版)[陈军][程序源代码]-GPS inertial navigation combinations (2nd Edition) [CHEN] [source code]
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这是关于GPS和惯性导航紧结合很好的资料,好不容易在网上收集的,有详细的算法。-This is the combination of GPS and inertial navigation tight good information, finally online collection, detailed algorithms
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严恭敏_博士学位论文
论文中采用激光陀螺捷联惯导系统为主导航系统,通过与里程计和气压高度计组合,构成车载自主定位定向系统,并借助路标点进行误差补偿。该定位定向系统不依靠 GPS,中途无须停车作零速修正,是一种全自主的导航系统,具有定位定向精度高、机动性好、可靠性高和寿命长等优点。 -In this thesis, laser gyro strapdown inertial navigation system (SINS)
is selected as core navigation s
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光纤陀螺误差建模与分析,北航惯性导航基础课程大作业,含matlab程序代码-FOG error modeling and analysis, Northern-based inertial navigation operations courses, including matlab code
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捷联式惯性导航的传递对准,使用matlab语言编写-Transfer alignment of inertial navigation
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捷联式惯性导航的导航结算程序,使用matlab语言编写-Strapdown inertial navigation navigation and settlement procedures
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捷联式惯性导航的轨迹发生器,使用matlab语言编写-Strapdown inertial navigation path generator
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捷联式惯性导航的角速率匹配,使用matlab语言编写-Strapdown inertial navigation of angular rate matching
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捷联式惯性导航的角速率匹配卡尔曼滤波,使用matlab语言编写-Strapdown inertial navigation of angular rate matching kalman filter
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利用参数辨识法提取相关对准参数,从而估计出陀螺漂移和数学平台偏角并进行补偿。仿真结果表明,开路罗经法对准具有较高的对准精度、较好的快速性,能够满足捷联惯导系统在静基座下实现自对准的要求。-Expressions of mathematical platform misalignment angles of the open-loop algorithm are derived and parameter identification method is
used to pick-up the
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本科毕业设计,应用于无人机惯性导航芯片的程序,包括陀螺仪,磁航向计和高度计,能输出10通道的惯性导航信息。有部分asm内容。-UAV chips used in inertial navigation procedures, including gyroscopes, magnetic heading gauge and altimeter, inertial navigation information can output 10 channels. Some asm content.
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GPS/SINS捷联式惯性导航系统的代码实现-GPS/SINS strapdown inertial navigation system code
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运用四元数方法进行捷联惯性系统的姿态解算,并由加速度计的数据和陀螺的数据计算导航参数-The four element method for strapdown inertial navigation system of the attitude calculation, and the accelerometer and gyroscope data data computation of navigation parameters
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