Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

Article ID

86Z21

Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

Karthik SP
Karthik SP
Vijay Desai
Vijay Desai
DOI

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.

Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

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
Karthik SP
Vijay Desai
Vijay Desai

No Figures found in article.

Karthik SP. 2014. “. Global Journal of Research in Engineering – A : Mechanical & Mechanics GJRE-A Volume 14 (GJRE Volume 14 Issue A1): .

Download Citation

Journal Specifications

Crossref Journal DOI 10.17406/gjre

Print ISSN 0975-5861

e-ISSN 2249-4596

Classification
Not Found
Article Matrices
Total Views: 4608
Total Downloads: 2485
2026 Trends
Research Identity (RIN)
Related Research
Our website is actively being updated, and changes may occur frequently. Please clear your browser cache if needed. For feedback or error reporting, please email [email protected]

Request Access

Please fill out the form below to request access to this research paper. Your request will be reviewed by the editorial or author team.
X

Quote and Order Details

Contact Person

Invoice Address

Notes or Comments

This is the heading

Lorem ipsum dolor sit amet, consectetur adipiscing elit. Ut elit tellus, luctus nec ullamcorper mattis, pulvinar dapibus leo.

High-quality academic research articles on global topics and journals.

Acceptance testing of Electro Hydraulic based Aircraft Actuator Using LabVIEW

Karthik SP
Karthik SP
Vijay Desai
Vijay Desai

Research Journals