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INSandGPS
- 捷联惯导GPS组合导航Kalman滤波器-SINS GPS Navigation Kalman Filter
SINS-Initial-Alignment-Method
- 本文提出了一种基于转动基座的快速估计平台失准角的初始对准方法，研究了扩展观测量的Kalman滤波算法，指出转动基座初始对准的可观测度优于传统最优二位置对准。-This paper presents a quick estimate based on rotating base platform misalignment angle of the initial alignment method to study the extended observations of the Kalman fi
ins2
- 捷联惯导系统的计算，给出了速度和经纬度的变化曲线。-The SINS calculation, given the speed and the latitude and longitude of the curve.
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.
trajectory-simulation
- 用于做GPS/SINS、或SINS导航时要用到的初始数据发生程序-For the initial data of GPS\/SINS, or SINS navigation to be used
Kara
- 通过外部观测位置速度信息，修正捷联惯导系统数据-Speed through external observation position information, correction data SINS
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.