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为了能较好地控制四旋翼飞行器的飞行姿态和和速度,采用位置式PID控制算法准确控制飞行器的飞行姿态。在proteus中进行硬件电路设计、仿真分析、通过合理的方案选材、调试论证、设计实现了四旋翼轴飞行器的样机模型。实验调试结果表明,使用位置式的PID控制算法可以根据实际情况灵活准确地调整四旋翼飞行器的飞行姿态,并准确的采集现场数据,因此,能更好地完成一些实际艰巨的任务。
In order to control the flight attitude and speed of quadrotor, the position PID control algorithm is used to control the flight attitude accurately. In the proteus hardware circuit design, simulation analysis, through a reasonable selection of programs, commissioning demonstration, design and implementation of a prototype four-axis quadcopter aircraft model. Experimental results show that using the position PID control algorithm can flexibly and accurately adjust the flight attitude of the quadrotor based on the actual situation and accurately collect the field data, so that some really difficult tasks can be completed better.