flight velocity

The simulation results of trimming calculation under the different flight velocity condition is conducted. The effect of trim results from different parameters is discussed. Graphical User Interface is designed using Matlab tool software.

运用matlab软件设计图形用户界面GUI，进行了无人直升机不同前飞速度下配平计算仿真研究，讨论了不同参数对配平结果的影响。

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Rotating speed spectrum are calculated from altitude-velocity characteristic, flight altitude and flight velocity.

然后根据发动机的高度速度特性和飞行高度与速度计算出该发动机的航线类转速谱。

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Its working state affects the flight velocity, tactics performance and flight security.

其工作状态直接影响飞机的飞行速度、战术性能的发挥及飞行安全。

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The mathematic model equations, boundary conditions and nonlinear iterative algorithm established herewith can be used to calculate the variations of flight path, velocity ( or angular velocity), acceleration as well as load factor, etc, with time for the said maneuvers.

所建立的数学模拟方程、边界条件以及非线性迭代求解方法，可以用来计算该机动科目的飞行轨迹、速度（或角速度）、加速度以及载荷因数等随时间的变化。

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To deal with the situations of close flight and cross flight, the velocity information of targets and the method of partly processing are taken into track correlation.

针对近飞目标和交叉飞行目标的情况，点迹与航迹的关联采用了分块处理技术，并融合了目标的速度信息。

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Time of flight velocity selector

飞行时间速度选择器

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The influence of the experimental conditions on the flight velocity of the ejected plasma was discussed based on the feature of their time-of-flight spectra.

结果表明，在脉冲激光沉积薄膜的情况下，喷射等离子体的飞行速度主要依赖于作用于靶面的激光能量密度。

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In addition, the effects of flight height, flight velocity, and radius of water droplet on droplet trajectories were also investigated.

此外，还研究了飞行高度、飞行速度及水滴半径对水滴撞击特性的影响；

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Emulational study on the effect on the cruise missile penetration by shortcut flight course, flight altitude and flight velocity

巡航导弹飞行捷径、高度及速度对突防影响的仿真研究

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A new method of flight velocity recognition of low-velocity projectile

低速弹飞行速度识别的一种方法

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at the global coordinate system, the flight velocity and flight angle of all the fragments are calculated with program.

在全局坐标系下，对所有破片的飞散速度和飞散角度进行了编程计算。

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One is velocity based multi-model predictive control method. Improvement is made on reference trajectory and switching rule to realize efficient large range tracking control of flight velocity.

一是研究了基于速度切换的多模型预测控制方法，通过对参考轨迹及切换准则的改进实现了对大范围速度指令信号的快速跟踪。

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Finally, the working loading spectra are calculated from altitude velocity characteristic, flight altitude and flight velocity.

最后根据发动机的高度&速度特性计算出发动机的工作参数谱。

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The rocket reaches the predicted flight velocity after the operation of booster is finished, then the sustainer starts work during which the thrust of rocket is equal to the resistance acting on the rocket, while the lift of the rocket is equal to its weight.

助推器工作结束后，火箭达到预定飞行速度，主发动机开始工作，使火箭的推力等于其所受阻力，同时火箭产生的升力等于其重力，保证火箭可等速飞行；

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The model's flight velocity is 4.8~ 5.7km/ s, and the chamber's pressure is 10~ 80mmHg.

球模型飞行速度为4.8～5.7km／s，靶压10～80mmHg。

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