Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

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Karthik SP

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Vijay Desai

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National Institute of Technology Karnataka

Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

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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.

References

7 Cites in Article

Reference Format

A Goldenberg,S Habibi (1999). A Mechatronics Approach for the Design of a New High Performance Electro Hydraulic Actuator.
G Daneker (1973). Army View of Acceptance Tests.
G Mcgrath (1964). What Is Acceptable Service Life?.
H Moon,W Knowles (1970). Acceptance Criteria for Demonstrating System Safety Requirement.
Pawel Rzucidlo (2006). Laboratory and Preliminary In-Flight Tests of Electromechanical Actuators.
Pawel Rzucidlo (2006). Laboratory and Preliminary In-Flight Tests of Electromechanical Actuators.
Shrinath S V Londhe,E M Jois,Peethambaran (1999). Vehicle Evaluation and Test System.

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Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

How to Cite This Article

Karthik SP. 2014. \u201cAcceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW\u201d. Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 14 (GJRE Volume 14 Issue A1): .

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GJRE Volume 14 Issue A1
Pg. 29- 34

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Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Keywords

Electro-Hydraulic (EH) and Smart Test Controller Unit (SCU)LabVIEW Portable Test Controller (PTC)

Submission ReceivedDecember 16, 2013
Peer Review Double Blind
Handling Editor
Accepted December 31, 2013
Published January 15, 2014

Version of record

v1.2

Issue date

March 2, 2014

Language

en

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Article Matrices

Total Score: 102

Country: India

Subject: Global Journal of Research in Engineering - A : Mechanical & Mechanics

Authors: Karthik SP, Vijay Desai (PhD/Dr. count: 0)

View Count (all-time): 214

Total Views (Real + Logic): 4696

Total Downloads (simulated): 2311

Publish Date: 2014 03, Sun

Monthly Totals (Real + Logic):

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Month 4: 53 views
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Total Views: 4696

Total Downloads: 2311

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Published Article

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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