Design of test system of aircraft DC power supply system based on LabVIEW

Author

Shutuan, Zhang ; Yi, Zhang ; Lingshun, Liu ; Yanli, Gao

Author_Institution

Naval Aeronaut. & Astronaut. Univ., Yantai, China

Volume

2

fYear

2011

Firstpage

255

Lastpage

258

Abstract

According to the requirement of the fast test for Aircraft DC power supply system, the test system of aircraft DC power supply system based on LabVIEW is designed in this paper. The test system mainly consists of the hardware system and the software system. The hardware part can realize the signal conditioning and high speed data acquisition. The software system based on LabVIEW adopts modular design ideas, and can accomplish the test data analysis and processing according to the GJB181 and GJB181A. The test system has been used in the parameter test of the aircraft DC power system in the outfield. It is shown that the test system not only has the character of high accuracy, but also easy to schlep. In addition, it displays a good and reliable performance that satisfies the test requirement for aircraft DC power supply system.

Keywords

aircraft power systems; data acquisition; power engineering computing; signal conditioning circuits; virtual instrumentation; GJB181A; LabVIEW; aircraft DC power supply system; hardware system; high speed data acquisition; modular design; signal conditioning; software system; Aerospace electronics; Aircraft; Application software; Data acquisition; Data analysis; Generators; Power supplies; Aircraft DC power supply system; Data analysis and processing; Parameter test; Virtual Instrument;

fLanguage

English

Publisher

ieee

Conference_Titel

Electronic Measurement & Instruments (ICEMI), 2011 10th International Conference on

Conference_Location

Chengdu

Print_ISBN

978-1-4244-8158-3

Type

conf

DOI

10.1109/ICEMI.2011.6037810

Filename

6037810