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建立了某型无人直升机的线性化模型,并对动态矩阵控制算法进行了相关的理论研究,结合经典的PID控制应用至某型无人直升机飞行控制系统控制律。经仿真验证,该设计方法可行、合理。
The linearization model of some type of unmanned helicopter is established. The related theories of the dynamic matrix control algorithm are also studied. The classical PID control is applied to the control law of a certain type of unmanned helicopter flight control system. The simulation shows that the design method is feasible and reasonable.