National Institute of Technology, Karnataka.To: Author

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RE86Z21
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This paper presents an approach to perform aircraft actuator Acceptance Testing capability. Efforts include design and development of Test system for Electro Hydraulic aircraft actuator, in nominal condition that may be used along with measurement data to generate effective test results. LabVIEW platform is used for developing the test system.To develop communication between the LabVIEW based Test software and Actuator, Portable Test Controller (PTC), is used.
Karthik SP, Vijay Desai. 2014. "Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW". Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 14 (GJRE Volume 14 Issue A1).
Crossref Journal DOI 10.17406/gjre
Print ISSN 0975-5861
e-ISSN 2249-4596
v1.2
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Total Score: 102
Country: India
Subject: Global Journal of Research in Engineering
Authors: Karthik SP, Vijay Desai (PhD/Dr. count: 0)
View Count (all-time): 332
Total Views (Real + Logic): 1083
Total Downloads (simulated): 68
Publish Date: 2014 01, Wed
Monthly Totals (Real + Logic):
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