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本文对航空发动机的双变量控制方法进行了研究 ,提出了一种非理想解耦自适应控制方法 ,各子系统之间部分残余的相互耦合和非线性影响就通过自适应律本身的鲁棒性来解决。仿真结果表明该控制系统实现了解耦控制 ,对发动机模型参数在大范围内的变化均有良好的控制效果。
In this paper, we study the aero-engine bivariate control method and propose a non-ideal decoupling adaptive control method. The residual residual mutual coupling and non-linear influence between the subsystems are achieved by the robustness of the adaptive law itself To solve. The simulation results show that the control system achieves decoupling control and has good control effects on the changes of engine model parameters in a wide range.