基于PID经典控制的小型无人直升机高度控制的研究

A high degree of control research to small unmanned helicopters based on the classic PID control

引用小型无人直升机简化模型,获得其高度控制的原理图。采用经典的PID控制法对其高度控制进行控制律设计,建立其精确的控制通道方块图。再利用matlab进行仿真调试,研究其高度控制。

The small unmanned helicopters used to simplify the model,its high degree of control over the schematic. Using the classic PID control law for control of its high degree of control law designed to establish the precise control of channel block diagram.Matlab for reuse simulation testing to study the high degree of control.