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Description
| - This paper describes a measurement system capable to test a vibration influence on navigation devices. The system consists of a signal generator, vibratory equipment, on which a reference sensor can be placed, and a PC. The system works with real flight acceleration data. A main idea of the system is to use original flight acceleration information from intervals with constant engine RPM, approximate it, and generate in the laboratory conditions. The approximation uses four strongest harmonics of the original acceleration evaluated by FFT analysis. The system for vibration tests is fully automatic and feed-forward, which allows analyze acceleration data, choose the acceleration magnitudes and frequencies based on FFT, and generate the flight vibration in the laboratory. The system enables automatic calibration of vibratory table. The system, the user interface, and the comparison between user selected data and measured data will be further presented and discussed.
- This paper describes a measurement system capable to test a vibration influence on navigation devices. The system consists of a signal generator, vibratory equipment, on which a reference sensor can be placed, and a PC. The system works with real flight acceleration data. A main idea of the system is to use original flight acceleration information from intervals with constant engine RPM, approximate it, and generate in the laboratory conditions. The approximation uses four strongest harmonics of the original acceleration evaluated by FFT analysis. The system for vibration tests is fully automatic and feed-forward, which allows analyze acceleration data, choose the acceleration magnitudes and frequencies based on FFT, and generate the flight vibration in the laboratory. The system enables automatic calibration of vibratory table. The system, the user interface, and the comparison between user selected data and measured data will be further presented and discussed. (en)
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Title
| - System for Vibration Testing
- System for Vibration Testing (en)
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skos:prefLabel
| - System for Vibration Testing
- System for Vibration Testing (en)
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skos:notation
| - RIV/68407700:21230/11:00183490!RIV12-MSM-21230___
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http://linked.open...avai/riv/aktivita
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http://linked.open...avai/riv/aktivity
| - P(GD102/09/H082), S, Z(MSM6840770015)
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http://linked.open...vai/riv/dodaniDat
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http://linked.open...aciTvurceVysledku
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http://linked.open.../riv/druhVysledku
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http://linked.open...iv/duvernostUdaju
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http://linked.open...titaPredkladatele
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http://linked.open...dnocenehoVysledku
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http://linked.open...ai/riv/idVysledku
| - RIV/68407700:21230/11:00183490
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http://linked.open...riv/jazykVysledku
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http://linked.open.../riv/klicovaSlova
| - vibration testing, electronic inclinometer, acceleration (en)
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http://linked.open.../riv/klicoveSlovo
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http://linked.open...ontrolniKodProRIV
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http://linked.open...v/mistoKonaniAkce
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http://linked.open...i/riv/mistoVydani
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http://linked.open...i/riv/nazevZdroje
| - MDS - Měření, diagnostika, spolehlivost palubních soustav letadel 2011 - Sborník příspěvků z 11.mezinárodní vědecké konference
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http://linked.open...in/vavai/riv/obor
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http://linked.open...ichTvurcuVysledku
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http://linked.open...cetTvurcuVysledku
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http://linked.open...vavai/riv/projekt
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http://linked.open...UplatneniVysledku
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http://linked.open...iv/tvurceVysledku
| - Roháč, Jan
- Šipoš, Martin
- Stach, Michal
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http://linked.open...vavai/riv/typAkce
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http://linked.open.../riv/zahajeniAkce
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http://linked.open...n/vavai/riv/zamer
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number of pages
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http://purl.org/ne...btex#hasPublisher
| - Univerzita obrany. Fakulta vojenských technologií Brno
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https://schema.org/isbn
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http://localhost/t...ganizacniJednotka
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