搜索资源列表
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
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。
imu_ahrs
- 基于IMU(三轴角速率、三轴加速计和三轴磁场)的方位姿态解算系统(ahrs)，基于C语言开发，VC 6.0编译器，可方便的移植到其他环境。-Based on the IMU (three-axis angular rate, three-axis accelerometer and three-axis magnetic field) to locate gesture Solution System (ahrs), based on C language development, VC 6.0
Navigation_integration_algorithm
- 最近在弄陀螺稳定，得到这篇很经典的资料，江南航天集团的。捷联式惯性导航积分算法。很稀罕的。-Get gyro stabilized recently received information of this classic, Jiangnan Aerospace Group. Strapdown inertial navigation integration algorithm. Very rare for.
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