利用飞行试验信号对发动机模型辨识进行了研究。
The engine model identification using flight test signals is introduced.
由这若干个小偏差动态模型组合成描述全工作范围动、静态特性的发动机模型。
These segments assembled the engine model with property of dynamic and static state in the whole operating range.
简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。
The mission section, the constrain conditions, the weight composition of the maneuverable missile, and the model of used in turbofan engine maneuverable missile were presented.
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