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1)  Fixed Wing AirVehicle
固定翼飞行器
2)  fixed-wing MAV
固定翼微型飞行器
3)  fixed-wing aircraft
固定翼飞机
1.
Based on the takeoff safety criterion,a ski-jump model was developed to predict a land-based ski-jump takeoff performance for a fixed-wing aircraft.
从固定翼飞机陆基滑跃起飞的安全性要求出发,提出了一种预测起飞性能的模型,用于预测最小起飞速度和最短滑跑距离。
2.
The method of flight path simulation of fixed-wing aircraft was studied based on the motion equation,with the help of which the flight path can be simulated and the location and flight attitude can be calculated.
研究了基于飞机运动方程的固定翼飞机航迹仿真方法,利用飞行器的运动方程进行固定翼飞机航迹模拟,建立飞机运动仿真模型算法,然后用MATLAB程序实现飞机航迹仿真,并对直线航迹和跑道型航迹进行了算法分析,最后将仿真航迹与真实航迹比对。
3.
Based on the features of torpedo airdropping by fixed-wing aircraft, the spatial vectoring patterns of instantaneous torpedo dropping were presented, and the mathematic model for dropping and aiming were established, as well as its calculation methods for direction aiming and distance aiming were analyzed.
针对固定翼飞机空投鱼雷的特点,给出了投雷瞬间的空间矢量图,建立了投放瞄准数学模型,分析了方向瞄准和距离瞄准的计算方法。
4)  rotorcraft [英]['rəutəkrɑ:ft]  [美]['rotɚ,kræft]
旋翼飞行器
5)  flapping wing air vehicle
扑翼飞行器
1.
In allusion to the flight control of flapping wing air vehicle(FAV), a method of design the flight controller for FAV based on linear estimation is presented.
针对扑翼飞行器(FAV)的飞行控制,提出一种基于近似线性化的控制方法。
6)  aircraft empennage
飞行器尾翼
1.
Starting from aircraft empennage’s non linear characteristic, the non linear reason is discribed,and the identification method of structure dynamic characteristic is discussed.
从飞行器尾翼非线性特征出发 ,描述了非线性成因 ,讨论了结构动态特性的辨别方法 。
补充资料:复杂气象飞行(见飞行技术)


复杂气象飞行(见飞行技术)
instrument meteorological conditions flight

fuza qixiangfe主xing复杂气象飞行(instrument meteorologiealconditions flight)见飞行技术。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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