最后采用算例直升机数据，根据提出的建模方法进行了定直飞行的配平计算和操纵响应分析，仿真结果证明了建模理论和方法的合理性和有效性。
Finally, the trim calculation and response analysis were carried out with the example helicopter's data. The simulation results validate the rationality and validity of modeling theories and methods.
最后采用算例直升机数据，进行了定直飞行的配平计算和操纵响应分析，结果证明了模型的合理性和有效性。
Finally the trim calculation and response analysis are carried out with the example helicopter's data. The results validate the rationality and validity of the model.
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