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1·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。

2·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。

3·The solution of nonlinear algebraic equations is usually met in the study of flight dynamics.

飞行动力学研究中常遇到求解非线性代数方程组的问题。

4·At last, some topics on advanced application of GPS re-lated with flight dynamics are put forward.

最后提出了作为GPS高级应用专题的飞行力学若干研究课题。

5·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。

6·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。

7·In this paper, the rotor power transfer coefficient is determined from the point of helicopter flight dynamics.

文章详细地介绍了从飞行力学的角度来确定直升机平直飞行时的旋翼功率传递系数。

8·Then a two-step method for the set-membership identification of a helicopter fully coupled flight dynamics model is established.

在此基础上，建立了直升机全耦合飞行动力学模型集员辨识的两步法。

9·In this article, a new method based on support vector machine (SVM) is proposed to identify the flight dynamics of SUHs at hover.

提出一种利用支持向量机(SVM)对SUH悬停动态进行辨识建模的新方法。

10·To acquire the climb track of Aero-Space Plane, it is established that the flight dynamics model of the Aero-Space Plane which takes off and lands.

为了获得优化的组合动力空天飞行器爬升轨迹，以一型水平起降空天运载飞行器为依托，针对任务剖面建立典型状态的飞行动力学模型。