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小型无人机飞行姿态串级控制系统
The system design of small unmanned aerial vehicle flight attitude control based on STM32
【摘要】 采用四元数互补滤波算法对IMU单元等多传感器采集到的数据进行解算融合,串级PID为小型无人机飞行姿态系统的控制算法。设计了实时监测子系统,实验结果表明,基于STM32的串级PID控制算法可以实现飞行姿态的有效控制。
【Abstract】 The quaternions complementary filter algorithm is used for data fusion,which are sampled from IMU unit and other sensors.Cascade PID algorithm is applied into the Unmanned Aerial Vehicle(UAV)pose control system with a real-time monitor.Experimental results indicate that the cascade PID algorithm based on STM32 is effective for the UAV pose control.
【基金】 吉林省科技厅基金资助项目(20170204038SF)
- 【文献出处】 长春工业大学学报 ,Journal of Changchun University of Technology , 编辑部邮箱 ,2017年05期
- 【分类号】V249.1
- 【被引频次】5
- 【下载频次】215