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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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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,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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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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这是一个有关低成本捷联惯性导航系统研究的论文,对有一定捷联惯性导航基础认识的同学学习很有帮助-This is a paper about low-cost strapdown inertial navigation system research, to have some basic understanding of SINS students learn helpful
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详细研究了捷联惯导系统的力学编排,仿真条件等,也包括各种理论知识-The strapdown inertial navigation system are studied in detail the mechanical arrangement, the simulation conditions, etc., also includes a variety of theoretical knowledge
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初始对准是捷联惯导系统进行导航的前提,初始对准的好坏将直接影响到系统的导航精度。捷联惯导系统(SINS)初始对准的本质是确定载体的初始姿态。-The initial alignment of strapdown inertial navigation system is the premise for navigation, initial alignment will directly affect the quality of the navigation system precision.
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捷联惯性导航系统的matlab仿真,还包含圆锥误差的补偿等。-Matlab simulation of strapdown inertial navigation system, including the compensation of the error of the cone, etc..
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matalab仿真的捷联惯导,写的比较清楚明白(Strapdown inertial navigation system based on MATALAB simulation)
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捷联惯导的详细介绍,附有编程程序供大家参考学习(Strapdown inertial navigation system in detail, with programming procedures for your reference learning)
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PSINS工具箱程序
适用于惯性导航仿真设计(Precise Strapdown Inertial Navigation System)
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捷联惯导算法、四元数算法姿态解算、误差补偿及仿真分析,matlab仿真程序(Attitude calculation of strapdown inertial navigation system algorithm based on Matlab)
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里面详细介绍了卡尔曼滤波算法及捷联惯导系统,并结合两者设计算法(The Calman filtering algorithm and strapdown inertial navigation system are introduced in detail, and the two design algorithms are combined.)
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