稳定性是飞机电源系统供电质量的重要指标。
Stability is an important target of the quality of an electrical supply in an aeroplane's a.
飞机高压直流电源系统是一种新型的飞机电源系统。
High voltage direct current (HVDC) aircraft electrical power generating system (EPGS) is a new type of aircraft power generating system.
多电飞机供电系统理论提出后，对飞机电源系统的工作可靠性等性能提出了更高的要求。
After the theory of the More Electric Aircraft Power Supply System is proposed, higher reliability is needed for the Aircraft Power Supply System.
飞机电源系统是飞机机载设备的重要组成部分之一，包括交流电源系统和直流电源系统。
Aircraft electric power source system (AEPSS) is an important part of aircraft equipment. AEPSS includes AC-AEPSS and DC-AEPSS.
该逆变电源并联控制技术已成功地运用于飞机电源系统中，实现了两台逆变电源的并联工作。
The control technology of parallel operating converter was put into use of practical aircraft power supply system successfully, and two inverters in parallel were realized.
目前飞机电源系统的性能检测主要还是采用人工测试的方法，往往需要耗费大量的人力、物力和时间。
Presently the performance test of the Aircraft power Supply System still relies on manual methods, which cause a waste of manpower, material resources and time.
发电机控制器(GCU)是飞机电源系统的控制中心，能实现对飞机电源系统的保护、控制及BIT功能。
The generator control unit (GCU) is the control center of the aircraft electrical power generation system (EPGS), GCU provides protection, control and BIT function for the EPGS.
以飞机电源系统为例，提出了互为热贮备系统的概念，并归纳出其可靠性的分析方法，指出了各种方法的使用条件。
Taking airplane power system for example, the conception of mutual heat reserve system is presented, the methods of reliability analysis and the working conditions of the system are introduced.
以飞机电源系统为例提出了一种在系统设计阶段，利用系统动态性能仿真模型自动进行定量故障模式影响分析的方法。
Advance an automatic quantitative analysis method of failure modes and effects analysis with system transient simulation in the system design stage, take a airborne power system as a case in point.
本文所设计的全数字控制器的硬件开发平台功能完善，性能好，通用性强，可以用于飞机电源系统以及电力系统的发电机控制器的研制和开发。
The general development platform has a good performance. It can be used to design new Generator Control Unit for aircraft power supply system or power system.
介绍了利用虚拟仪器技术设计、开发的飞机电源参数测试仪，它可对多种机型的电源系统的供电参数进行测量。
The power supply parameters measuring apparatus for airplane developed by the technology of virtual instrument is briefly introduced in this paper.
介绍了利用虚拟仪器技术设计、开发的飞机电源参数测试仪，它可对多种机型的电源系统的供电参数进行测量。
The power supply parameters measuring apparatus for airplane developed by the technology of virtual instrument is briefly introduced in this paper.
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