某型无人机俯仰角控制回路的控制律设计

Design for the control law of a UAV pitch angle control loop

文章以某型无人机为研究对象,利用经典控制理论的知识,分析根轨迹,对无人机的俯仰运动的相关控制律进行了设计,并在SIMULINK软件中进行仿真验证,证明其控制律的有效性、正确性。

The article sets a UAV as the research object,with the knowledge of classical control theory analyzes the root locus,on the pitch movement of the UAV control law design and simulation in the SIMULINK software,to prove the effectiveness of the control law,correctness.