The control surface plate timely and clearly shows work status of dry regeneration. 预结晶除湿干燥机控制面板实时显示干燥再生工作状态,一目了然。
A modified linear quadratic optimal controller is designed for the linear part, while adaptive gain is used in the nonlinear part for adapting to different control surface damages. 线性部分采用改进的线性二次型最优控制器法进行计算,而非线性部分采用自适应增益来更好地适应故障情况。
The Aeroelastic Flutter and Its Active Control of a 2-D Airfoil with a Control Surface 带操纵面二元机翼的气动弹性颤振及其主动抑制
Theoretical analysis and simulation results for fighter's control surface faults show that the presented method is effective. 理论分析和针对歼击机在机动飞行过程中各种舵面故障的仿真研究均表明本文方法的有效性。
Aerodynamically balanced control surface 空气动力平衡操纵面
It is very important and difficult to control surface quality of cold rolled and hot dip galvanized strip from the strip produced by CSP. CSP工艺生产的热轧卷作为冷轧原料生产冷轧镀锌产品的表面质量较难控制。
Measuring the hinge moment of aircraft's control surface is a important task for the flight test. 测量飞机舵面铰链力矩是飞行试验的一项重要任务。
Flight control surface actuator 操纵面致动装置舵机
It is essential for flight control reconfiguration to obtain on-line information of the control surface failures as they will influence the controllability of an aircraft. 舵面故障会影响飞机的操纵性,为实现飞机的控制重构需在线诊断出舵面的故障信息。
A Nonlinear PD Controller and Its Control Surface Rotating 一种非线性PD控制器及其控制面旋转
This paper studies the active flutter suppression of the two-dimensional airfoil with control surface by using ultrasonic motor as the actuator. 本文采用超声电机作为作动器来实现含控制舵面的二元机翼的颤振主动抑制。
Based on different forms of hinge points and rocker-arms, four local models of control surface linkage forms were proposed. 根据舵面悬挂点与摇臂操纵形式的不同,提出了四种连接方式的局部模型。
The computed results of its aerodynamic characteristics and flight performance show that this new configuration concept of control surface for maneuverable warhead is feasible. 气动特性和飞行性能计算评估结果表明,这种新的机动弹头气动舵面布局理念是可行的。
Most compositions, such as scene system, flight system, flight's sound and control surface are all simulated. 模拟了飞机的主要系统:飞行系统、视景系统、仪表系统和音响系统。
Influence of Control Surface Characteristics on Short Period Mode Flying Qualities for Flying Wing Aircraft 舵面特性对飞翼构型作战飞机短周期品质的影响飞翼布局飞行器副翼性能及重构分析
The rudder is a control surface that steers and stabilises the boat. 舵是控制表面,公牛和稳定的船。
A variable control surface on the trailing edge of an aircraft wing, used primarily to increase lift or drag. 襟翼飞机后翼上最初用来增加上升力或拖力的可灵活控制的辅助翼。
We consider robust controller design problem of a class of linear systems for actuator and control surface damage, we presented tolerant robust controller design method. 对执行器故障和控制面故障情况,提出了容错的鲁棒控制器的设计方法。
The aerodynamic forces on any control surface produce a moment about the hinge. 在任何操纵面上的空气动力均产生围绕其铰链轴的力矩。
Study on the Control Surface Characteristics and Flight Control of the High Sweepback Flying Wing UAV 大后掠飞翼布局无人机操纵面特性及控制研究
Unsteady Transonic Flow Computation for a Wing with Control Surface Deflections by Euler Equations 跨声速机翼操纵面非定常气动力Euler方程计算
Remember, you don't have direct control over the amount or direction of control surface deflection. 记住,你并没有直接操作控制面偏转的方向和大小。
This paper presents a ALGOL program for Calculating The lift distribution on wings with control surface in steady and unsteady subsonic flow. 本文提供了计算亚音速偏转操纵面机翼的定常和非定常升力分布的算法语言程序。
The analytical results indicate that the control surface efficiency analyzed based on nonlinear experimental aerodynamic forces and linear theoretical aerodynamic forces are different. 研究表明:使用非线性试验气动力和线性理论气动力所分析得到的舵面效率具有较大的差别;
Effect of Control Surface Freeplay on Nonlinear Aeroelastic Responses of an Airfoil 控制面间隙对非线性二元机翼气动弹性响应的影响
Composite material repair for various structural parts of aircraft, such as Radome, flight control surface, etc. 雷达罩、操作舵面等飞机部件日常复合材料修理工作。
A Simple Adaptive Reconfigurable Control Method for Aircraft Control Surface Loss-of-Effectiveness Failures 飞机舵面损伤的简单自适应重构控制方法
A short, winglike control surface projecting from the fuselage of an aircraft, such as a space shuttle, mounted forward of the main wing and serving as a horizontal stabilizer. 鸭式飞机的水平安定面和升降舵:从一架飞行器伸出的一个短的翼状控制平面,如航天飞船的机身,被安在飞机翼前方,作为水平稳定器。
Hopf bifurcation analysis is employed to investigate the problems of the control surface buzz. 采用Hopf分叉分析方法,对跨音速操纵面嗡鸣问题进行了研究。
Applicable range of this model and way for improving control surface efficiency have been pointed out. 指出数学模型的适用范围和改善操纵面效率的途径。