Simulations on the nonlinear model of the twin spoolturbojet engine aerothermodynamics are conducted to verify the disturbance rejection and tracking performance.
所述方法在某型双转子涡喷发动机气动热力学非线性模型上对抗干扰性和目标跟踪进行了仿真验证。
2
As an example, a robust control law is designed to the twin-spoolturbojet engine system using the given method. The result shows that the given method is feasible.
文中以双转子涡喷发动机控制器设计为例，设计了基于LMI的鲁棒控制器，结果表明所给方法是可行的。
3
A brief view and results of tests for the effects of the inlet total pressure distortion on the performance and the stability of a two-spoolturbojet engine are presented.