Search - strapdown navigation matlab

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[matlab] sins_alignment DL : 0: 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.
Update : 2025-02-17 Size : 2kb Publisher : 吉庆昌
[File Format] jinglianguandaofangzhen DL : 0: 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
Update : 2025-02-17 Size : 2.79mb Publisher : lele
[Books] StrapdownInertialNavigationIntegration DL : 0: 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.
Update : 2025-02-17 Size : 196kb Publisher : huzhou
[Other] INS DL : 0: 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!
Update : 2025-02-17 Size : 1.02mb Publisher : 罗云峰
[Multimedia Develop] naviga090205 DL : 1: 捷联惯性导航的仿真程序用四元数法的捷联惯性导航姿态解算程序资源大小:...用四元数法进行姿态解算的matlab程序-Strapdown inertial navigation simulation program
Update : 2025-02-17 Size : 20kb Publisher : ww
[source in ebook] SINS-code-matlab DL : 0: 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
Update : 2025-02-17 Size : 1kb Publisher : 小何
[Other] sins-code-navigation DL : 0: 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
Update : 2025-02-17 Size : 3kb Publisher : 小何
[matlab] 796e50c2-1775-4730-8213-2225004ca5c1 DL : 0: 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.
Update : 2025-02-17 Size : 102kb Publisher : 宋磊
[Software Engineering] MATLAB DL : 0: 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
Update : 2025-02-17 Size : 474kb Publisher : 宋磊
[Other] strapdown DL : 0: 捷联惯性导航解算程序，内附实测数据与说明文档-Strapdown inertial navigation solution counting procedures, and inserting the measured data and documentation
Update : 2025-02-17 Size : 375kb Publisher : 魁
[Communication-Mobile] GPS_INS0914 DL : 0: 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.
Update : 2025-02-17 Size : 7kb Publisher : zhanglaoshi
[Other] jingtai DL : 0: 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.
Update : 2025-02-17 Size : 3.75mb Publisher : 秋叶
[transportation applications] F16 DL : 0: 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
Update : 2025-02-17 Size : 193kb Publisher : pei fu-jun
[source in ebook] SINS_Kalman DL : 0: 捷联惯性导航系统、GPS/SINS组合导航系统仿真程序-Strapdown inertial navigation systems, GPS/SINS Integrated Navigation System Simulation Program
Update : 2025-02-17 Size : 468kb Publisher : xiatao
[matlab] strapdown DL : 0: 惯性导航捷联算法的matlab实现，内附举例坐标点。-Strapdown inertial navigation algorithm matlab implementation, enclosing the coordinates of points, for example.
Update : 2025-02-17 Size : 117kb Publisher : 熊志珲
[matlab] trace DL : 0: 这是模拟飞机飞行的不同阶段的轨迹程序，比较全面，可用于捷联和组合导航的数据来源-This is a simulated flight trajectory of the different stages of process, more comprehensive, can be used in strapdown and navigation data sources
Update : 2025-02-17 Size : 5kb Publisher : yyh
[matlab] Strapdown DL : 0: 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
Update : 2025-02-17 Size : 392kb Publisher : 袁刚平
[matlab] Alignment DL : 0: Matlab code for Strapdown navigation system alignment-Matlab code for Strapdown navigation system alignment.
Update : 2025-02-17 Size : 945kb Publisher : rhongxiang
[matlab] Strapdown-algorithm-matlab DL : 0: 捷联惯导程序，依据加表和陀螺仪的输出数据来求解飞行器的姿态-Strapdown inertial navigation algorithm matlab
Update : 2025-02-17 Size : 11kb Publisher : lizhihua
[Other] SINS-MATLAB DL : 0: 惯性导航程序,matlab程序, 有注释,很不错的参考程序(strapdown navigation matlab code)
Update : 2025-02-17 Size : 9kb Publisher : chenpeng3361

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