2015
DOI: 10.1016/j.proeng.2014.12.631
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The Test Verification Design Method Based on Rapid Prototyping Technology of Aero-engine

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Cited by 5 publications
(3 citation statements)
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“…They can handle even the most complex tasks simple and flexibly. 27 Control of the devices (LEDs, fluorescents, etc.) connected to the analog input unit of the NI CompactRIO 9075 is accomplished by transferring data from the analog output unit (current sensor, light sensor, etc.)…”
Section: Hardware Construction Of the Studymentioning
confidence: 99%
“…They can handle even the most complex tasks simple and flexibly. 27 Control of the devices (LEDs, fluorescents, etc.) connected to the analog input unit of the NI CompactRIO 9075 is accomplished by transferring data from the analog output unit (current sensor, light sensor, etc.)…”
Section: Hardware Construction Of the Studymentioning
confidence: 99%
“…Along with the pursuit of faster, safer and more convenient demands, people are paying more attention to flight safety. As to the aircraft failure, more than 50% of accidents are reported to come from the engines, while the gas path failure could account for 90% of the total engine failure [6]. High speed fuel solenoid valve (HFSV) is an important control element in the aerospace field, which is mainly used in aero-engine guide vane regulating systems [7,8].…”
Section: Introductionmentioning
confidence: 99%
“…Full digital simulation 3 and hardware-in-the-loop (HIL), for example, are two typical beforehand verifications in the whole development workflow of the control system. [4][5][6] Following HIL, semi-physical testing is crucially important for final verification before cell testing. In this testing, all other physical components except an engine mathematical model can be used.…”
Section: Introductionmentioning
confidence: 99%