1) manipulation effects
操纵效应
2) reversal of control
操纵无效
3) control reversal
操纵反效
1.
This paper aims at presenting an investigation into aerodynamics and control reversal characteristics of adaptive wings with seamless, variable camber, flexible trailing edge.
对后缘可无缝、连续柔性偏转的自适应机翼进行了二元气动特性和操纵反效特性分析。
4) control power
操纵效能
1.
Requirement characteristics of low-aspect-ratio combat flying wings' roll axis control power
小展弦比飞翼战机滚转轴操纵效能需求特性
2.
Roll axis and yaw axis control power requirements of roll maneuver,crosswind takeoff and landing,asymmetric thrusts were studied,and in some cases the control power requirements of combat flying wings are quite different with those of the conventional-configuration combat airplanes,due to the disappearance of vertical tail and rudders and the appearance of the new-style control effectors set.
随着控制系统对系统动态特性调节作用的日益增强,由飞机构型所引起的动态响应特性差异已变得越来越小,飞翼飞机的闭环滚转模态、螺旋模态、滚转-螺旋耦合振荡、荷兰滚模态、驾驶员座位处的侧向加速度等均可达到较好的飞行品质,但稳态配平特性主要受构型的影响,不能完全满足飞行品质的要求;分析了大展弦比飞翼作战飞机在快速滚转、侧风起降和非对称推力情形下的对滚转轴和偏航轴操纵效能的要求,由于气动构型和操纵面配置等差异,大展弦比飞翼作战飞机在完成某些飞行任务时对操纵效能的需求与常规构型的飞机存在着较大差异。
5) control response
操纵响应
1.
Based on the model,research of the steady control response of SA349 baseline ECR is conducted.
以此为基础,对SA349基准电控旋翼的稳态操纵响应进行了计算分析。
2.
Taking the WZ-1 as the example helicopter, the trim and control response were calculated, and comparison between the ECR helicopter and the normal one was done.
以WZ-1直升机为样例直升机,对比分析了电控旋翼直升机与常规直升机的配平特性和操纵响应特性。
3.
Based on the model,according to the parameters of a medium type autogyro,the trim and control response characteristics are calculated.
在此基础上,根据某中型旋翼机基本参数,对该机进行了配平及操纵响应特性计算。
补充资料：电传操纵系统(见飞机人工飞行操纵系统)
电传操纵系统(见飞机人工飞行操纵系统)
fly-by-wire control system
dianehuan cuozongx认ong电传操纵系统(fzy一by一wir。。。n:r。，system)见飞机人工飞行操纵系统。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条