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1)  force directed
力矢量
1.
It is resulted from the combination of the core growth and the force directed algorithm,the core growth algorithm is served to install the core cells with some sub-core cells all around to reduce the length of interconnecting wire,the force directed algorithm computes the force among cells to adjust the optimization of placement.
结合核心生长和力矢量算法的思想,构成核心生长-力矢量(CGFD)算法来实现门阵列模式布局。
2)  thrust vector
推力矢量
1.
Investigation on a thrust vector design scheme of ramjet;
一种冲压发动机推力矢量设计方案研究
2.
Design of thrust vector measuring system for engine;
发动机推力矢量测试系统的设计
3.
Researches of dorsal support interference in low speed wind tunnel thrust vector test;
低速风洞推力矢量试验背撑干扰特性试验研究
3)  Thrust vectoring
推力矢量
1.
Attitude control of thrust vectoring unmanned aerial vehicle based on brain emotional learning
基于大脑情感学习的推力矢量无人机姿态控制
2.
A study on the integrated flight and propulsion control system(IFPCS) with the thrust vectoring for a cer-tain type of unmanned aerial vehicle(UAV) is carried out.
以某无人机为背景,主要研究大机动时带推力矢量的综合飞行/推进控制系统的设计方法。
3.
The design of the flight control system with the thrust vectoring is discussed.
研究了带推力矢量飞机过失速非线性飞行控制问题。
4)  thrust vector control
推力矢量
1.
In this paper,six degrees of freedom model of air-to-air missile is established by using bank to turn(BTT) and the thrust vector control(TVC) technologies.
应用倾斜转弯(Bank to Turn,BTT)及推力矢量控(ThrustVector Control,TVC)技术设计并建立了空空导弹六自由度模型。
2.
Three-kind thrust vector control (TVC)rudder systems are briefly introduced.
简要介绍了三类推力矢量舵系统,分析了几种主要推力矢量舵系统的操作效率。
5)  thrust-vector
推力矢量
1.
The aerodynamics design process of jet vane of the thrust-vector motor is discussed by combining the practical engineering.
结合工程实际,论述和分析了推力矢量发动机燃气舵气动特性的设计过程。
2.
The aerodynamic properties of thrust-vectoring et vane are studied by six-component forces test and all the forces on the vane flake and the force moments around the vane flake axes are obtainted.
采用六分力试验技术对某推力矢量发动机燃气舵的气动特性进行了试验研究。
6)  vector thrust
矢量推力
1.
This paper considers UCAV with vector thrust(UCAVVT)as research object,builds a flight dynamic model of UCAVVT and a flight control model of missile guide as research base.
无人战斗机逃逸概率是无人机设计的重要指标之一,提高无人机飞行时的可用过载能够提高其逃逸概率,另外无人机的机动也对其逃逸概率有重要影响,如何评判在各种机动情况下无人机对导弹的平均逃逸概率与其过载的关系是无人机设计师和军方十分关注的问题;论文以带矢量推力无人战斗机(UCAVVT)作为研究对象,建立其飞行动力学及导弹导引飞行控制数学模型,通过预先假定无人机做典型机动的概率,由计算机仿真导弹与无人机的相对飞行轨迹,研究讨论在各种机动下UCAVVT在导弹攻击下的平均逃逸概率,并对计算结果进行了分析,得出了一些重要结论,对带矢量推力无人战斗机的总体设计具有一定的参考价值。
补充资料:赤力力
1.亦作"赤历历"。 2.象声词。
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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