电传操纵

现代电传操纵飞机驾驶员手操纵器试飞演示

Advanced Fly-By-Wire Aircraft Pilot 's Hand Controller Flight Test Demonstration

电传操纵系统台架检测仪的研制

Research of a detecting instrument for the platform of fly-by-wire control system

采用NI公司的LabWindows/CVI软件开发平台，通过ODBC实现LabWindows/CVI和VISUALFOXPRO数据库之间共享数据，设计了某型飞机电传操纵系统联调试验台，并介绍了使用Agilent34970A数据采集/开关单元进行数据采集的方法。

By using LabWindows / CVI from NI Corporation and Visual FoxPro database , a testbed for Fly-By-Wire ( FBW ) control system , which use ODBC technique is given . Method on how to use Agilent 34970A data acquisition / switch unit to acquire data is also introduced here .

本文以装备纵向数字电传操纵系统（DFBW）的某验证机为实例，分析研究了该人-机闭环系统中驾驶员模型参数变化和可能出现的操纵差错对纵向着陆品质的影响。

By taking a verifying aircraft which is equipped with longitudinal DFBW as an example , this paper studied of influences to landing flying qualities for probable controlling mistake and pilot model parameters variations in the man-aircraft closed-loop system .

电传操纵系统设计中遇到的突出问题和对策

In design of few control system meet with protrusive problem and countermeasure

飞机电传操纵系统多余度电液舵机运动同步性的测试与调整

Synchronization Testing and Adjustment of the Multi-Channel Electro-hydraulic Servo Actuator

基于PC/104总线的电传操纵系统检查仪设计

The ATE Based on PC / 104 Bus of Fly-By-Wire Control System

电传操纵飞机起飞着陆动态特性仿真研究

A simulation study on takeoff and landing dynamics of fly-by-wire control system aircraft

电传操纵系统在民用客机中的新发展

New Development in the Fly-by-wire System of Civil Airliners

在目前的电传操纵系统中，普遍采用被动驾驶杆系统。

At present , passive side-stick system is mostly used in fly-by-wire system .

基于行为的故障诊断方法在某型飞机电传操纵系统中的应用

Applications of an Behavior Based Fault Diagnosis Method in Flight_by_Wire System of an Aircraft

飞机电传操纵系统安全性分析方法的研究

Study on System Safety Analysis Methods of the Fly by Wire System of Aircraft

某型飞机电传操纵系统联调试验台的研制

Design of a testbed for fly-by-wire control system

电传操纵系统可靠性分析及飞行安全评估

The Reliability Analysis of Fly-By-Wire Flight Control System and Flying Security Evaluation on the Horizontality

光传操纵系统是针对传统电传操纵系统的不足提出的一种新型的飞控系统。

The Fly-by-Light ( FBL ) system is proposed for the shortage of the traditional Fly-by-Wire controlsystem .

以电传操纵作为显著特征的第三代飞机飞行试验具有极大的挑战性和风险性。

As the3rd generation fighter , primarily characterized by fly-by-wire , FBW aircrafts flight testing owns great challenges and risks .

得出的结论对研究人-电传操纵系统-飞机组合系统的驾驶员诱发振荡问题也是有益的。

These results are also useful in the study of the PIO problem of " men-Fly by control system-aircraft " synthetic system .

某型飞机电传操纵系统四余度电液舵机模拟器设计电液余度数字阀在船舶液压舵机系统中的应用研究

The Simulator Design of the Four-channel Electro-hydraulic Servo Actuator Applied Research on the Electro Hydraulic Redundancy Digital Valve in Marine Hydraulic Steering Gear

为了解决传统电传操纵系统抗电磁干扰能力差、带宽低等问题，提出了飞行控制系统光传方案。

A fly-by-light flight control system was developed to replace the fly-by-wire system which is susceptible to electromagnetic interference and has low bandwidth .

针对某型飞机电传操纵系统台架在检查维护中存在的耗时、易出错等缺点，本文研制了一种基于虚拟仪器技术的台架检测仪。

Based on virtual instrument (ⅵ) technology , a new detecting instrument has been designed for the platform of fly-by - wire ( FBW ) control system .

在航空航天飞行器设计中，随着主动控制技术、随控布局及电传操纵系统的普遍采用，飞行控制系统的地位变得更为重要。

With widespread adopting of the Active Control Technique ( ACT ) and Control Configuration Vehicle ( CCV ) and Fly-by - wire system , position of Flight ControlSystem ( FCS ) become even more significant .

可靠性是飞机设计的重要指标，现代民用飞机电传操纵系统的伺服作动系统普遍采用余度技术，传统的可靠性分析方法无法描述其动态过程。

Reliability is an important index for civil aircraft . Servo-actuation systems for modern civil aircraft with FBW ( fly-by-wire ) use redundancy technology widely and traditional methods of reliability analysis cannot describe their dynamic process .

采用最优控制驾驶员模型在频率域内分析是理论评价电传操纵飞机着陆下滑状态飞行品质的一种有效方法。

Optimal control pilot modeling technique in frequency domain analysis is an effective methodology used to analytically evaluate the handling qualities of aircraft with fly by wire flight control systems in the approach and landing task .

然后建立机械操纵系统、电传操纵系统的数学模型，并编制非线性全量时域仿真程序，对起飞着陆动态特性做出了综合的全面的定量分析，其结果与试飞情况吻合。

The mathematical models of mechanical control system and fly-by-wire control system are provided . The nonlinear time domain computer program provides a complete quantitative analysis of aircraft takeoff and landing dynamics , and the numerical simulation results agree well with the real flight test data .

使用等效系统评价方法，根据数值计算结果分析了全权限电传操纵飞机从小迎角到失速迎角横航向飞行品质对于气动参数变化的灵敏度。

By use of the equivalent low order system matching method , sensitivity of the lateral and directional flying qualities of all authority , fly by wire aircraft ( FBW a / c ) to variations of aerodynamic parameters was investigated from low up to stall angles of attack .

介绍了重型设备运载车的转向机构型式和5种转向模式，要实现这5种转向模式，必须将轮轴设计成机械上相互独立的形式，独立和多轮转向机构只能采用电传操纵方式。

This paper introduces the steering mechanism structure of heavy equipment carrier and 5 steering modes . The wheel shaft must be designed mechanically and independently each other to realize these 5 steering modes , the independent and multi - wheel steering mechanism can use electric driving control mode only .

简单介绍了主动控制技术（ACT）电传飞行操纵余度系统可靠度预测的方法。

The work for predicting Reliability of Ely-By-wire FCS for Active control technique ( ACT ) is also presented .

现代飞机上普遍装备了先进的飞行控制系统，采用电传伺服操纵，取代了最初的机械式人力操纵。

Modern aircraft equipped with advanced flight control systems has replaced the role of the manpower operational vehicles at the initial stage of the power flight history .

概括和总结了中国飞行试验研究院利用变稳飞机在电传飞机飞行试验中所完成的研究工作及其重要意义；针对电传操纵，重点描述了对PIO的飞行试验研究以及试飞员培训等。

It describes and summarizes some important research work of the variable stability aircraft in the FBW flight test , primarily expatiating on the flight tests of PIO , HAOA , ASE and test pilot training .