搜索资源列表
SINS-MATLAB-simulation-program-source-code
- 捷联惯导仿真程序MATLAB源代码，能帮助大家了解捷联惯导原理-SINS MATLAB simulation program source code, can help you understand the principles of the SINS
sins
- 捷联与平台惯导静基座初始对准程序,C语言编写，很好的例程-Strapdown inertial navigation static base and the platform initial alignment process, C language, a good routine
55593417JIELIAN
- c语言的版的捷联惯导,很牛的，请大家分享啊-c initial alignment using the North East to coordinate system, 10 state variables
mti_calibrated
- 一个非常全面的捷联惯导程序，包含了从初始对准、初值的设定，四元素的四阶龙格库塔法更新，对速度微分方程和位置方程分别用龙格库塔法和欧拉角法求解-A very comprehensive program SINS, including from the initial alignment, initial set, the four elements of the fourth order Runge-Kutta method updates the location of the speed di
mine2
- 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.
MsinsGPS
- 这是低精度光纤捷联惯导与GPS组合的博士论文,内容丰富,希望对需要的人有用!-This is a low-accuracy fiber-optic strapdown inertial navigation and GPS combination of doctoral dissertation, rich in content, in the hope that those who need it useful!
strap_down_inertial_navigation
- 捷联系统C语言实现算法，已经过实验验证。-SINS C language algorithm, has been verified by tests.
fangzhenshuju
- 捷联惯导系统仿真数据生成工具，可以用来验证捷联算法-SINS simulation data generation tool that can be used to verify Inertial Algorithm
jielian
- 捷联惯导仿真程序。针对于一般飞行器应用的捷联惯导系统，选择以地理坐标系为导航坐标系，根据指北方位系统的导航原理进行力学编排及数值仿真；制导系统针对于一般的弹道导弹，设计标准弹道，比较摄动制导与显式制导的优劣性，选择灵活性较好、适应性较强的显式制导，以待增速度为关机函数，控制关机，使之命中目标。-sins simulation
matlab
- matlab应用于捷联惯导系统初始对准滤波技术程序-matlab applies SINS initial alignment procedures Filtering Technique
INSandGPS
- 捷联惯导GPS组合导航Kalman滤波器-SINS GPS Navigation Kalman Filter
796e50c2-1775-4730-8213-2225004ca5c1
- 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
chushiduizhuncanshubianhua
- 捷联惯性导航的算法，去掉两个参数后的改进算法- The initial alignment of SINS
Navigation_integration_algorithm
- 最近在弄陀螺稳定，得到这篇很经典的资料，江南航天集团的。捷联式惯性导航积分算法。很稀罕的。-Get gyro stabilized recently received information of this classic, Jiangnan Aerospace Group. Strapdown inertial navigation integration algorithm. Very rare for.
GPS_INS111
- 捷联惯性导航与GPS组合导航的matlab实现。采用自适应算法来对组合导航时行处理，并取得了很好的效果。
GPS_INS0914
- 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.
dongtai
- 捷联惯导的C程序实现，四元数表示姿态，动态数据显示，MATLAB进行图像处理，包含原始数据。-SINS of the C program implementation, said the attitude quaternion, dynamic data, MATLAB for image processing, including raw data.
jingtai
- 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.
xiaotuoluo
- 捷联惯导的C程序实现，四元数进行姿态更新，MATLAB进行图像处理，包含原始数据。-SINS of the C program implementation, quaternion for attitude update, MATLAB for image processing, including raw data.
guijishuju
- 捷联惯性导航的姿态数据自动生成，利用C程序实现，可用于验证接连导航程序。-Posture of strapdown inertial navigation data automatically generated using the C program implementation, can be used to verify the series of navigation program.