Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

Authors

  • Karthik SP

  • Karthik SP

  • Vijay Desai

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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How to Cite

Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW. (2014). Global Journals of Research in Engineering, 14(A1), 29-34. https://testing.engineeringresearch.org/index.php/GJRE/article/view/980

 
Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

Published

2014-01-15

Issue

Vol. 14 No. A1 (2014): GJRE-A Mechanical and Mechanics: Volume 14 Issue A1

Section

Articles

License

Copyright (c) 2014 Authors and Global Journals Private Limited

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW. (2014). Global Journals of Research in Engineering, 14(A1), 29-34. https://testing.engineeringresearch.org/index.php/GJRE/article/view/980