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1)  vertical tailless aircraft
无垂尾构型
1.
In this paper, the design of an adaptive control system of the vertical tailless aircraft with thrust vectoring control was presented, and the problem of output trajectory control of the typical input-output feedback linearizable nonlinear dynamic system by state variable s feedback is considered.
研究了采用自适应控制系统的无垂尾构型推力矢量飞机的飞行控制性能。
2)  V-shape vertical tail
V型垂尾
3)  vertical tail
垂尾
1.
In the traditional assembly technology of aerofoils and vertical tails, the measurement of pose and print of the specified points are realized by the indicator of horizontal points and elastic striker respectively, which is not precise and difficult to be flexible.
在传统的机翼、垂尾装配中,姿态测量与测量点打制分别由特别设计的水平测量点指示器和弹簧打点器实现,不仅精度不高,而且难于实现柔性化。
2.
According to the phenomenon of vertical tail vibration divergence encountered during development test of an air- craft,a study on the flutter analysis and vibration data measured in flight test are performed.
针对某型机调整试飞中遇到的垂尾发散振动现象,对该机的颤振分析和试飞实测数据进行了研究。
4)  dart configuration
后尾式构型
5)  tailless model
无尾型,全翼型
6)  DISA upright boxless moulding
DISA垂直无箱造型
补充资料:因梦得题公垂所寄蜡烛因寄公垂
【诗文】:
照梁初日光相似,出水新莲艳不如。
却寄两条君领取,明年双引入中书。
[宰相入朝举双烛,余官各一。]





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【出处】:
全唐诗
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