搜索资源列表
InertialNavigation
- 捷联导航相关知识，陀螺，及速度及惯性敏感器件和测试、补偿标定技术以及捷联系统算法的相关知识-Strapdown navigation knowledge, gyro, and speed and inertia-sensitive devices and tests, calibration and compensation algorithms SINS knowledge
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.
strapdown
- 自编的SINS仿真Matlab程序，对初学者还算全，应该有点用处，虽然比较简单，也省些前期编写的麻烦-The SINS self-compiled Matlab simulation program, for beginners fairly full, it should be somewhat useful, though relatively simple, but also save some trouble of pre-prepared
strapdown
- 捷联惯导源程序，matlab编写 捷联惯导源程序，matlab编写-SINS source code, matlab write SINS source, matlab write
test2
- 捷联更新 matlab 仿真 捷联惯导 控制导航-Strapdown update matlab simulation SINS control 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
SINS-VelAlignment-time-delay-MATLAB
- 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 ~
SINS
- 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 ~
shixiong
- GPS/SINS捷联式惯性导航系统的代码实现-GPS/SINS strapdown inertial navigation system code
SINS-algorithm
- 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
low-cost-sins
- 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
KF
- 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.
SINS-zitaijiesuan
- 捷联惯性导航领域的姿态更新算法仿真，包括二子样、三子样和四子样的对比。-In the field of strapdown inertial navigation attitude updating algorithm simulation, including two sample, the third and the fourth kind of contrast.
SINS
- 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..
chuandiduizhun
- 捷联惯导系统传递对准matlab程序,已经验证过，非常好用(matlab sins Transfer alignment of strapdown inertial navig)
sins
- 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)
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)
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