Description: 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. Platform: |
Size: 2048 |
Author:吉庆昌 |
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Description: 捷联惯导系统仿真算法的研究及其实现.nh.大连理工大学硕士论文，详细阐述了如何用matlab-simulink进行惯导仿真-Strapdown inertial navigation system simulation algorithm and its realization. Nh. Dalian University of Technology master s thesis in detail how to use matlab-simulink simulation for INS Platform: |
Size: 2929664 |
Author:lele |
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Description: This paper provides a rigorous comprehensive approach to the design of the principal software
algorithmsutilized inmodern-day strapdown inertial navigationsystems: integration of angular rate into attitude,
acceleration transformation/integration into velocity, and integration of velocity into position. Platform: |
Size: 200704 |
Author:huzhou |
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Description: 这是一本关于无陀螺捷联式惯性导航的书籍，具有很高的参考价值！-This is on a non-gyro strapdown inertial navigation books, have a high reference value! Platform: |
Size: 1064960 |
Author:罗云峰 |
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Description: 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 Platform: |
Size: 1024 |
Author:小何 |
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Description: 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 Platform: |
Size: 3072 |
Author:小何 |
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Description: 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 and the attitude quaternion matrix solvers such as the use of programming" gyroscope and accelerometer Modeling used. Platform: |
Size: 104448 |
Author:宋磊 |
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Description: 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 Platform: |
Size: 485376 |
Author:宋磊 |
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Description: 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. Platform: |
Size: 7168 |
Author:zhanglaoshi |
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Description: 捷联惯惯性导航的C程序实现，四元数表示姿态，静态下进行试验，MATLAB进行图像处理，包含原始数据。-Strapdown inertial navigation of the C programs used to achieve, said the attitude quaternion, static tests under, MATLAB for image processing, including raw data. Platform: |
Size: 3934208 |
Author:秋叶 |
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Description: F16飞行控制仿真程序，主要是利用matlab/simulic对F16建模并对其飞行条件进行仿真-Strapdown inertial navigation static base and the platform initial alignment process, C language, a good routine Platform: |
Size: 197632 |
Author:pei fu-jun |
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Description: 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中保存的为比力信息f_INSc(单位m/s^2)、陀螺仪角速率信息wib_INSc(单位rad/s)，排列顺序为 一~三行分别为东、北、天向信息.
4: 航向角以逆时针为正。
5:地球椭球长半径re=6378245 地球自转角速度wie=7.292115147e-5 重力加速度g=g0*(1+gk1*c33^2)*(1-2*h/re)/sqrt(1-gk2*c33^2)；
g0=9.7803267714 gk1=0.00193185138639 gk2=0.00669437999013 c33=sin(lat纬度) -First, data on:
1: inertial navigation system that links the north bit of the Czech system. Initial longitude 116.344695283 degrees latitude 39.975172, height h is 30 meters.
Initial speed of v0 = [0.000048637 0.000206947 0.007106781], the same altitude.
2: jlfw for 600 seconds of data, gyroscopes and accelerometers were sampling period of 1/80 sec and 1/80 seconds.
3: Initial attitude angle [0.120992605 0.010445947 91.637207] (pitch, roll, heading, in units of degrees),
jlfw than the power saved information f_INSc (unit m/s ^ 2), angular rate gyro information wib_INSc (units of rad/s), in the order of 1 ~ three lines were east, north, days to the information.
4: The heading angle is positive counterclockwise.
5: Earth ellipsoid long radius re = 6378245 Earth s rotation angular velocity wie = 7.292115147e-5 acceleration due to gravity g = g0* (1+ gk1* c33 ^ 2)* (1-2* h/re)/sqrt (1-gk2* c33 ^ 2)
g0 = 9.7803267714 gk1 = 0.00193185138639 gk2 = 0.00669437999013 Platform: |
Size: 401408 |
Author:袁刚平 |
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Description: 基于Matlab的捷联惯导轨迹发生器，希望给大家有所帮助-Strapdown inertial navigation trajectory generator based on matlab。May be help to you Platform: |
Size: 4096 |
Author:haha |
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Description: 基于圆锥误差补偿算法和划船误差补偿算法的等效原理，可将圆锥误差补偿算法移植到划船误差补偿对圆锥误差补偿算法和捷联惯导算法进行了仿真。给出了Matlab的m文件源程序代码具有一定的参考价值。
-Based on the coning error compensation algorithm and the sculling error compensation algorithm of equivalent principle, the coning error compensation algorithm of transplanted to rowing error compensation of coning error compensation algorithm in strapdown inertial navigation algorithm and simulation was carried out. Gives the Matlab a m file source code has a certain reference value.
Platform: |
Size: 7168 |
Author:春晓 |
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Description: 捷联惯性导航系统的matlab仿真程序 主要是针对飞行器 或者汽车 舰船-Matlab simulation of strapdown inertial navigation system program for aircraft or automobile ship Platform: |
Size: 2048 |
Author:lilei |
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Description: 关于捷联惯性导航传递对准的仿真程序，期待学术交流~谢谢分享~-Simulation program on Transfer Alignment of Strapdown Inertial Navigation and look forward to the academic exchange ~ Thank you for sharing ~ Platform: |
Size: 4096 |
Author: |
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