DocumentCode
2518351
Title
16-channel PC-based aircraft electrical power monitor
Author
Harris, Joseph M. ; Levin, Richard J. ; Santamaria, Juan C.
Author_Institution
Georgia Tech Res. Inst., Georgia Inst. of Technol., Atlanta, GA, USA
fYear
1993
fDate
18-20 May 1993
Firstpage
637
Lastpage
642
Abstract
The authors describe a system developed to monitor the outputs of the primary electrical power sources on the HH/MH-60G PAVE HAWK helicopter. The system is capable of simultaneously monitoring the output voltage and current from two direct current power sources. This capability corresponds to sixteen channels of data including two DC voltage channels, and six AC current, six AC voltage channels, and six AC current channels. The primary purpose of the monitoring system is to evaluate the electrical loading on the power sources, as a function of time, during helicopter flight operations. However, it can also be configured to evaluate short term events, such as transients, on a reduced number of channels
Keywords
computerised monitoring; electric current measurement; helicopters; load (electric); microcomputer applications; power system measurement; voltage measurement; HH/MH-60G PAVE HAWK helicopter; PC-based aircraft; electrical loading; electrical power monitor; helicopter flight; output current; output voltage; primary electrical power sources; short term events; transients; Aircraft manufacture; Analog-digital conversion; Helicopters; Military aircraft; Monitoring; Portable computers; Power system transients; Sensor phenomena and characterization; Software design; Voltage;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation and Measurement Technology Conference, 1993. IMTC/93. Conference Record., IEEE
Conference_Location
Irvine, CA
Print_ISBN
0-7803-1229-5
Type
conf
DOI
10.1109/IMTC.1993.382565
Filename
382565
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