以此为基础，建立了电控旋翼直升机的飞行动力学模型。
Then the flight dynamics model of the ECR helicopter was constructed.
主要研究舰载飞机在进场下滑着舰过程中的飞行动力学问题。
The flight dynamics problems in the process of aircraft approach glide—down and landing are studied.
主要研究舰载飞机在进场下滑着舰过程中的飞行动力学问题。
The flight dynamics problems in the process of aircraft approach glide—down and landing are studied.
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