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two spool turbojet 双转子涡轮喷气发动机
two-spool turbojet 双级压缩机涡轮喷气发动机
twin-spool turbojet 双转子涡喷发动机
twin spool turbojet 双转子涡喷发动机
one spool turbojet 单转子涡轮喷气发动机
one-spool turbojet 单转子涡轮喷气发动机
double spool turbojet 双转子压气机的涡轮喷气发动机
single-spool turbojet 单级压缩机涡轮喷气发动机
a twin-spool turbojet 双转子涡喷发动机
Simulations on the nonlinear model of the twin spool turbojet 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。
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.
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。
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-spool turbojet engine are presented.
介绍进气总压畸变对双轴涡喷发动机性能和稳定性影响的试验及其结果。
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