産業用大型マルチコプタシミュレータの開発

抄録

In this research, we are built an attitude control simulator for a large industrial multicopter. Therefore, we build on a simulator for maintaining quadcopter levels. First, the simulator of the block diagram of attitude control model of roll axis is built. We observe the step response and replace the existing PID parameters used to fly the simulator to the actual simulator created. In the evaluation of its stability, we evaluate the rise time and the amount of overshoot. In addition, you can find the poles of the characteristic equation for the entire transfer function throughout the simulation block diagram. The stability of the controlled object is analyzed by looking at the poles. By adjusting existing PID parameters and investigating PID parameters with better transient characteristics, a more stable simulator is built.