1.
Parameters Test for the Aircraft Power Supply System Based on Personal Computer and Software Engineering;
基于PC机下飞机供电系统参数测试及软件设计
2.
Reliability Analysis of Mutual Heat Reserve Airplane Electric Power Systems
互为热贮备飞机供电系统的可靠性分析
3.
Advanced aircraft power system and its control system was introduced and fault tolerant design of data bus was discussed.
介绍了先进飞机供电系统及其控制系统的组成，并对数据通信总线的容错设计进行论述。
4.
Playing an essential part in the aeroplane power supply system, they must be strictly tested before they are dispatched from the factory to ensure their quality.
它们是飞机供电系统中的重要部件,为了保证质量,在出厂前必须对其进行严格的测试。
5.
spacecraft power supply
太空飞行器供电系统
6.
Power System Processor( PSP) and Electric Load Manage Center( ELMC) are the important contents of research of the power distribution for more electric airplanes.
供电处理机和负载管理中心是先进飞机配电系统研究的重要内容。
7.
HELP (Helicopter Electronic Landing Path )
直升飞机电子着陆系统
8.
Systematic Research on the Airplane GCUBIT;
飞机电源GCU BITE系统研究
9.
The Study of Optimization on Shenyang Aircraft Corporation Commercial Airplane Material Supply System;
沈飞公司民用飞机物料供应系统优化研究
10.
Development of Hydrodynamic Drive Device for an Aircraft Ejection Fuel Feed System
飞机燃油引射供输油系统动流源研制
11.
Our worldwide corporate membership includes airframe and engine manufactures, avionics and systems integrators, suppliers and consultants.
工业界的会员包括飞机机体，发动机制造业，航空电子设备和系统集成商，供应商和顾问公司。
12.
Worldwide supplier of military and commercial airframe, engine, avionics and related test equipment, tooling and ground support equipment for fixed wing and helicopters, both military and commercial.
军用和商用飞机机体、动机、空电子及相关的试验设备，工具制造和地面保障系统的供应商。
13.
The airplane has a sophisticated electronic guidance system.
这架飞机有一套尖端的电子导航系统。
14.
Research on Aircraft All-electric Braking HIL Simulation System;
飞机全电刹车HIL仿真系统的研究
15.
Harmonic Test System for Aircraft Power System Based on Mallat Algorithm
基于Mallat算法的飞机电网谐波检测系统
16.
Application and Design of CAN Bus in Aircraft Power Distribution System
CAN总线在飞机配电系统中的应用设计
17.
Electric Loading Test System for Aircraft Rudder
飞行器舵机电动加载测试系统的研究
18.
A Study of Torque Control System of Switched Reluctance Motor for More-Electric Aircraft
多电飞机开关磁阻电机转矩控制系统研究