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SIM_IMU
- 惯性导航算法,实现陀螺仪的仿真,用于陀螺选型-inertial navigation algorithm, and the simulation gyroscope for gyro Selection
Kalman_sgm
- 卡尔曼滤波器，敏感器组合形式为数字太阳敏感器+磁强计+速率陀螺，具体的参数物理含义请见文件中的注释，航天人依旧一目了然-Kalman filter sensor combinations for the digital sun sensor+ magnetometer+ rate gyroscope, specifically the physical meaning of parameters see comments in the file, astronauts still at a gl
STIM202
- 该文档描述了STIM202三轴陀螺仪的特性特征，在角度测量方面比较精确-This document describes the STIM202 axis gyroscope characteristic feature accurate angle measurement
kalman_wwh
- 实现GPS/INS组合导航解算位置、速度、航向等参数。输入数据：东向位置、北向位置、航向角（度）、gps速度、陀螺仪角速度、里程计脉冲数-Implement integrated GPS/INS navigation solution position, speed, course and other parameters. Input data: east position, north position, heading angle (degrees), gps speed, angular
IMU
- 采用加速度计和陀螺仪互补滤波获得载体三维姿态。-Using accelerometer and gyroscope carrier complementary filter to get 3 d pose.
L3G4200D
- 陀螺仪的具体工作过程，指的是在无人机行业的应用-Detailed work process of gyroscope, refers to the application of unmanned aerial vehicle (uav) industry
Attitude-Algorithm
- 两种基于互补滤波的姿态算法，对陀螺仪和加速度计进行数据融合，解算姿态。一种使用了梯度下降算法，另一种使用反馈修正和李雅普诺夫分析。-Two algorithms for attitude estimate based on complementary filtering. Data form Gyroscope and Accelerometer are fused. One is based on gradient descent algorithm while the other is ba