fbw

Architecture Analysis And Development Of Distributed FBW Flight Control System

分布式电传飞行控制系统结构发展及分析

Induced Oscillation of Man Vehicle Closed System of FBW Aircraft

电传飞机人机闭环系统的诱发振荡

Flying qualities analysis for an aircraft with longitudinal analog FBW flight control system

某机纵向电传控制系统飞行品质分析

This paper have play of consult for design of FBW control system and improving aircraft behaviors .

对飞行品质的影响等做了较为充分有益的探讨。这对电传系统设计和改善飞行品质有参考作用。

Phase compensation for FBW system

电传系统的相位补偿

Design and realization of a FBW flight test stand for certain aircraft based on LabWindows / CVI

基于LabWindows/CVI的某型飞机FBW飞行试验台设计与实现

The quality of the FBW joint is mainly decided by temperature field distribution , process parameters during upsetting and the structure defects .

影响闪光焊接头性能的最主要因素包括焊缝区域的温度场分布、闪光顶锻的工艺参数和焊缝区域出现的缺陷组织。

Monte Carlo method is employed in longitudinal stability enhanced control law design and simulation process of a FBW flight control system in this paper .

设计过程也表明，蒙特卡罗方法可以有效支持和优化电传飞控系统的设计和验证过程。

In-Flight Simulation and FBW Aircraft Flight Tests

空中飞行模拟与电传飞机飞行试验

This paper presents the analysis and comparisions between the designed parameters of analog FBW flight control system and the results from flight testing .

本文概括地介绍某机纵向模拟式电传飞行控制系统参数设计与飞行品质试验研究的对比分析。

The flying qualities of the aircraft with FBW FCS is determined by the varied parameters of the system .

具有电传飞行控制系统的飞机，其飞行品质取决于系统参数。

A direct current flash butt welding ( DC FBW ) process is analyzed for an ultra fine grain steel using finite element method .

对超细晶粒钢直流闪光对焊过程进行了有限元分析。

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

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。

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

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。

Based on the indispensable flight technologies , this article made a deep research and studies on the important roles and uses of variable stability aircraft ( in-flight simulation ) in the FBW flight test .

从电传飞机飞行试验所必需的飞行试验技术出发，研究和探讨了变稳飞机（空中飞行模拟器）对电传飞机飞行试验的重要性和特殊作用；

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 .

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。

Based on the explicit model-following Fly-By-Wire ( FBW ) control system of the helicopter ( MFCS ), a real-time semi-physical nap-of-the-earth platform is established and a simulated fly test is processed .

在直升机显模型跟踪电传飞行控制系统（MFCS）的基础上，开发了直升机贴地飞行波分复用光传系统实时半物理仿真验证平台。

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 .

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。

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 .

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 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 .

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。