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Mti
- 惯性测量组件Mti进行数据采集，利用陀螺和加速度计数据进行捷联姿态角解算，采用四元数更新算法，解算周期可调。
trajection
- 用Matlab编写的轨迹发生器，输入初始的位置速度，姿态角，姿态变化等信息，模拟得到陀螺仪输出和加速度计的输出-Written with the Matlab path generator, enter the initial position, velocity, attitude, attitude changes and other information, the simulated gyro output and the output of the accelerometer
sins
- 该程序包括了飞行器轨迹计算、陀螺和加速度计的采样输入、以及由四元素解算出的飞行器姿态、位置、速度-The program includes the aircraft trajectory calculation, the sampling gyro and accelerometer input, and the solution calculated by the four elements of aircraft attitude, position, velocity
GY_80_9axi_BMP085
- 陀螺及加速度计和压力计组合成的方位解算软件，51单片机实现的解算。方位较为准确。-The azimuth gyroscope and accelerometer and manometer combined into solver software, to 51 MCU solver. The orientation is more accurate.
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.
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
psd-glpu
- matlab功率谱图，可以通过它对陀螺仪或加速度进行噪声误差分析，已经取得很好效果，请放心使用-matlab power spectrum, it can be a gyroscope or an acceleration noise error analysis, we have achieved very good results, ease of use