Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW
Keywords:
LabVIEW, Portable Test Controller (PTC), Electro-Hydraulic (EH) and Smart Test Controller Unit (SCU)
Abstract
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.
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Published
2014-01-15
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Copyright (c) 2014 Authors and Global Journals Private Limited
This work is licensed under a Creative Commons Attribution 4.0 International License.