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L002951
- 遗传算法在捷联惯导初始对准中的应用研究 遗传算法在捷联惯导初始对准中的应用研究-Genetic Algorithms in SINS Alignment of research on genetic algorithm in SINS Alignment of Study of Genetic Algorithms in SINS Alignment of the Applied Research
slipe
- 捷联惯导系统传递对准MATLAB程序，固定点平滑新算法。
GPSmatlab
- matlab 捷联惯导算法 matlab 捷联惯导算法 -SINS algorithm matlab matlab matlab algorithm of SINS SINS SINS algorithm matlab algorithm
gpsins
- 姿态解算程序，用于捷联惯导系统的姿态解析算法-Attitude solution procedures for the sins of attitude analytic method
gorithm
- 捷联惯导系统姿态测量算法SINS attitude determination algorithm-SINS attitude determination algorithm
a-new-method-for-moving-SINS
- 本文在运载体运动情况下，提出了一种适用于捷联惯导系初始对准的新算法，该算法以 惯性空间为参考基准，将初始对准姿态矩阵的实现分解为三部分-This movement of the transporter, the paper presents a system for SINS Initial Alignment of the new algorithm to inertial space as the reference point, the realization of initial a
Track_S
- 导航四元素法捷联惯导的四元素算法捷联惯导的四元素简单算法-strapdown inertia navigation
sins-MATLAB
- 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 al
DXsinscal_JZ
- 这是一个捷联惯导算法matlab程序。首先读入数据，然后进行解算，其中先使用等效旋转矢量进行姿态计算，再进行速度、位置解算，循环进行直至数据结束。-This is a matlab process of sins.
qk_AG
- 捷联惯导卡尔曼滤波算法初始对准，参考哈工程的硕士写的，效果可以，但是不知道观测量是如何构造的。-Kalman filter algorithm SINS initial alignment, Master of Engineering Reference Kazakhstan write, the effect can be observables but do not know how to construct.
secondexalign
- 该算法用于实现静基座二位置捷联惯导初始对准-The algorithm used to implement static base two position SINS initial alignment
navi
- 该算法利用matlab实现指北方位捷联惯导解算过程-The algorithm uses matlab achieve refers northern bit SINS solver process
newSINS
- 关于惯导算法的一般程序，主要针对捷联惯导-Inertial navigation algorithm general procedures for SINS
INStoolSim
- 里面主要是捷联惯导算法程序，另外还有很多例子可供参考-strap inertial navigation systerm
SINS
- 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)
编程
- 依据加计和陀螺仪的输出数据来求解飞行器的姿态(The attitude of the aircraft is solved by the output data of the addition and gyroscopes)
捷联惯导算法与卡尔曼滤波原理讲义（1017）
- 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.)
ecef+sins
- 代码1用于将位置经纬高信息转换为地心地固坐标系下xyz信息；代码2是捷联惯导算法代码，用于将加速度计和陀螺仪输出的信息进行解算得到位置、速度和姿态信息。(Code 1 is used to convert the location of warp and weft information into XYZ information in a geocentric coordinate system; code 2 is a strapdown inertial navigation algorit
捷联惯导算法与组合导航原理讲义（20180206）
- 本书主要讨论捷联惯导系统算法方面的有关问题，包括姿态算法基本理论、捷联惯导更新算法与误差分析、组合导航卡尔曼滤波原理、捷联惯导系统的初始对准技术、组合导航系统建模以及算法仿真等内容。希望读者参阅之后能够对捷联惯导算法有个系统而深入的理解，并能快速而有效地将基本算法应用于解决实际问题。(This book mainly discusses the algorithms of sins, including the basic attitude algorithm theory, the sins
daohangthree
- 西工大研一惯性测量实验的粗对准程序以及图示，参考《捷联惯导算法与组合导航原理讲义》(Coarse alignment procedure and graphics for the INS experiment of Xigong University of Technology, refer to the Lecture on Strapdown Inertial Navigation Algorithms and Integrated Navigation Principles.)