A method is presented for unmanned helicopter flight dynamics model identification.

研究了一种无人直升机飞行力学模型辨识方法.

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Then the flight dynamics model of the ECR helicopter was constructed.

以此为基础,建立了电控旋翼直升机的飞行动力学模型.

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This paper introduces the research and application of flight dynamics in design of control augmentation system.

介绍了飞行力学在某型飞机控制增稳系统设计中的研究和应用.

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According to the flight - dynamics theory, a mathematical model of aircraft ramp ski - jump take - off is established.

根据飞行动力学理论, 建立了 舰载 机滑跃起飞数学模型.

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