实验结果对于正确使用该类型双转子涡喷发动机具有重要的现实意义。
The experimental result has practical significance for correctly using the twin-rotor turbojet.
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。
Simulations on the nonlinear model of the twin spool turbojet engine aerothermodynamics are conducted to verify the disturbance rejection and tracking performance.
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。
As an example, a robust control law is designed to the twin-spool turbojet engine system using the given method. The result shows that the given method is feasible.
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