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flight qualities
相关语句
  飞行品质
     Control law is designed for plane in given situation for flight qualities.
     利用传统的控制律设计方法——根轨迹法,在满足飞行品质的条件下,设计飞机在给定状态点的控制律。
短句来源
     EQUIVALENT SYSTEMS METHOD TO EVALUATE THE FLIGHT QUALITIES
     评定飞行品质的等效系统法
短句来源
     To obtain the better flight qualities, many modern control methods are applied in the design of aircraft flight control systems.
     为了获得更好的飞行品质,许多现代控制方法被应用到飞机飞行控制系统中。
短句来源
     To obtain the better flight qualities, many modern control methods are applied in the design of aircraft flight control systems.
     为了获得更好的飞行品质,许多现代控制方法被应用到飞机飞行控制系统中。
短句来源
     This paper discribes status of the development of some flight dynamics problems in the modern fighter design,such as agility design guidelines and combat agility management system , post stall flight envelope expansion and maneuvers,high alpha flight control law design,thrust vectoring control and quasi tailless flight, high alpha characteristic analysis methods open and closed loop characteristic bifurcation analysis methods,and flight qualities requirements at high angles of attack.
     阐述了现代战斗机研制中若干飞行力学问题研究现状,内容涉及敏捷性设计指南和空战敏感性管理系统、过失速飞行包线扩展和机动飞行、大迎角飞行控制律设计、推力矢量控制和准无尾飞行、大迎角特性分析方法——开环和闭环特性分支分析方法和大迎角飞行品质要求六个方面。
短句来源
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  “flight qualities”译为未确定词的双语例句
     The calculation and analysis of a fighter roll performance in full envelope is presented. The reference flight state of the fighter is n_(y0)=0~0.8nymax. And the related flight qualities are checked by using military specification MIL-F-8785C.
     本文在全包线范围内,计算分析了某战斗机基准飞行状态为ny_0=0~0.8ny_(max)情况下的滚转性能,并用美国军用规范《MIL-F-8785C》的相应条款对比作了品质检查,最后给出了几点结论和看法。
短句来源
  相似匹配句对
     EQUIVALENT SYSTEMS METHOD TO EVALUATE THE FLIGHT QUALITIES
     评定飞行品质的等效系统法
短句来源
     Longitudinal Flight Qualities for Small Amplitude Precision Control
     用于小幅值精确控制的纵向飞行品质准则
短句来源
     The Flight of Youth
     飞逝的青春
短句来源
     Bird flight
     鸟类的飞翔(英文)
短句来源
     On the Qualities of Teachers of P.E.
     论体育教师素质
短句来源
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  flight qualities
The alternative design is more complex to build but exhibits improved flight qualities.
      
Although slightly more complex to build than the pointed-nose design, this airplane features improved flight qualities.
      


The calculation and analysis of a fighter roll performance in full envelope is presented. The reference flight state of the fighter is n_(y0)=0~0.8nymax. And the related flight qualities are checked by using military specification MIL-F-8785C. Finally, some conclusions and remarks are given.

本文在全包线范围内,计算分析了某战斗机基准飞行状态为ny_0=0~0.8ny_(max)情况下的滚转性能,并用美国军用规范《MIL-F-8785C》的相应条款对比作了品质检查,最后给出了几点结论和看法。

The model following technique is used in the design of longitudinal control law for a fighter in this paper. The technique is a control law design method which can specify the flight qualities prior to the design. A simple and appropriate iterative method to solve the control law gains is presented and some results of calculation and conclusions are given.

本文采用了可以预先确定飞行品质的控制律设计方法即模型跟踪法,对某战斗机的纵向控制律进行了设计,提出了一种简单且适用的求解控制律增益的迭代方法,同时给出了部分计算结果和结论。

This paper analyses and studies effects of pilot stress, control power and damping on flight qualities of helicopter, the simplify engineering computation formula for pilot gain and pilot assessments have been direved, and the results compare with flight test data. The results show that the technique in this paper is suitable to any helicopter flight test and design estimate.

本文分析和研究了驾驶员工作负荷、操纵功效和阻尼等对贴地飞行时直升机飞行品质的影响,导出了简化的驾驶员增益和驾驶员评定等级的工程计算公式,并与飞行试验数据进行了比较.结果表明,本文的方法可用于各种直升机的飞行试验和设计估算.

 
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