Software Test Engineer

CURRICULUM VITAE

KOTEESWARAN M Mobile No : 095********

E-mail : ***************@*****.*** Office No : 088******** PROFESSIONAL SUMMARY:

3.5 Years of Experience in Avionics Software Testing.

Involved in Software Testing of Mission Critical Avionics Systems.

Involved in Testing of HUD, SSDU, MFD and AHRS Units of LCA Tejas.

Working as a Software Test Engineer at AERONAUTICAL DEVELOPMENT AGENCY Research And Development Ministry of Defence, Bangalore. Deputed From M/S BUSINESS SOLUTION INTERNATIONAL From April 2019 To Till date.

Worked as a Software Test Engineer at AERONAUTICAL DEVELOPMENT AGENCY Research And Development Ministry of Defence, Bangalore. Deputed From M/S AJA FACTECH SERVICE PVT. LTD From Sep 2017 To Mar 2019.

Worked as a Electronics Engineer at BHARAT ELECTRONICS LIMITED, Ministry of Defence Bangalore. Deputed From M/S TRANSCCON INTERCONNECTION SOLUTION PVT. LTD From Jan 2017 To July 2017.

EXPERIENCE SUMMARY:

Experience in Low Level Testing (LLT), High Level Testing (HLT), Hardware Software Integration Testing

(HSIT) and Verification & Validation (V-Model).Worked on IBM RTRT Tool on DO-178B Standards in Aerospace Projects.

Good understanding of Software Development Life Cycle (SDLC) and Software Test Life Cycle (STLC).

In Software Testing, the Modified Condition & Decision Coverage (MC/DC) is a code coverage criterion that requires all of the below during Testing.

Design, build, and maintain efficient, reusable, and reliable C code.

Familiarity with continuous Integration Testing, Functional Testing, Automation and Manual Testing.

Ability to write Test Script, Test Case & Test Procedure.

Team player and Accustomed to fast paced environment, changing priorities & Multitasking. TECHNICAL SKILLS:

Operating System : Windows XP

Programming Languages : C

Tools : Rational Test Real Time, MS Visual C++, MATLAB

Communication Protocols : RS 232, RS 422, MIL-STD-1553B

Avionics Software Standard : DO-178B

WORKING EXPERIENCE :

PROJECT - 1 : HEAD UP DISPLAY (HUD)

Team Size : Four

Programming Languag : C

Tools : IDE VC++ 6.0, MATLAB, ORCAD

Project Description : The Tejas is an indigenous Light Combat Aircraft (LCA). LCA cockpit has many display units the Head Up Display (HUD) is an important cockpit display that is used to display the information received from the Open Architecture Computer (OAC) in a visual form by writing it on to a CRT screen which will be collimated and combined with the real world image through beam combiners. Role & Responsibilities:

Black Box Testing of Head Up Display .

Requirement Analysis, Development and Implementation of Dual Scan Raster Card for HUD.

Functional Testing, Integration Testing, Fault debugging, Certification and Documentation of HUD in both System level and Aircraft level.

Software Updating to Head Up Display Simulator.

Pre-installation & Functional Testing of Head Up Display Coordination with QA&SEG and HAL (CRI).

Co-ordination with QA&SEG, HAL (CRI) and RCMA (CEMILAC) for the Unit Clearance for Aircraft.

System design for testing of Head up Display Mk-1 and MK-2.

Creating schematics Design using ORCAD.

Post Flight Data Analysis and report generation for the Aircraft Flight Test Point clearance.

Having good knowledge on Flight data analysis using Matlab. PROJECT – 2 : SMART STANDARD BY DISPLAY UNIT (SSDU) Team Size : Four

Programming Language : C

Tools : IDE VC++ 6.0, RTRT

Project Description : The Smart Standby Display Unit is stand-alone color display unit. SSDU displays page information based on the parameters received through RS422. The SSDU is a high-end display system provided in the cockpit of LCA for the display of GET U HOME (GUH) parameters and ENGINE FUEL INDICATOR parameters (EFI). The same can act as GUH or EFI. SSDU shall function as SSDU_GUH or SSDU_EFI in TEJAS fighter and also as repeater SSDU_GUH and repeater SSDU_EFI in rear cockpit of TEJAS Trainer, depending on the function selection discrete inputs received through its external interfaces during POWER ON.

Role & Responsibilities:

CSU and CSC level testing of SSDU software using RTRT tool to perform White Box Testing for new version of SSDU.

Development and execution of test case, Unit & Component testing and generate test report.

Preparation of test document and Report Clearance document of Smart Standby Display Unit.

Conducting Black Box Testing for SSDU_GUH, SSDU-EFI.

Co-ordination with QA&SEG, HAL (CRI) and RCMA (CEMILAC) for the Unit Clearance for Aircraft.

Post Flight Data Analysis and report generation for the Aircraft Flight Test Point clearance.

Having good knowledge on Flight data analysis on SSDU and AHRS using Matlab. PROJECT - 3 : MULTI FUNCTION DISPLAY (MFD)

Team Size : Four

Programming Language : C

Tools : IDE VC++ 6.0

Project Description : The Multi Function Display (MFD) is a part of the Human Machine Interface

(HMI) between pilot and aircraft as display and control terminal. The MFD unit is a 5’’ by 5’’ color video display that forms a part of aircraft cockpit integrated display system. It has a high-resolution color Active Matrix Liquid Crystal Display (AMLCD) screen, capable of displaying a variety of display pages. TEJAS aircraft has three Multi Function Displays : Left Multi Function Display (LMFD), Center Multi Function Display (CMFD) and Right Multi Function Display (RMFD).

Role & Responsibilities:

Black Box Testing, Display Integration Rig Maintenance and Certification activity of MFD.

Involved Software updating and release Multiple Version of Software with respect to customer requirement.

Pre Installation & Functional Testing of Multi-Functional Display Coordination with QASEG & HAL (CRI).

Co-ordination with QA&SEG, HAL (CRI) and RCMA (CEMILAC) for the Unit Clearance for Aircraft.

Having good Experience on Multi Function Displays & Good debugging and analytical skills. ACADEMIC RECORD

Bachelor of Engineering in Electronics & Communication Engineering, St. Peter’s College of Engineering And Technology (Anna University), Chennai, Tamil Nadu. Percentage : 6.51(CGPA)

Year Of Passing : 2016

HSC - Indian Matriculation Higher Secondary School in Harur, Tamil Nadu. Percentage : 85

Year Of Passing : 2012

SSLC - Government Higher Secondary School, in Vaniyambadi, Tamil Nadu. Percentage : 80

Year Of Passing : 2010

PERSONAL DETAILS:

Father’s Name : Mahalingam K

Mother’s Name : Govindhammal M

Date of Birth : 02-May-1995

Gender : Male

Languages Known : English, Kannada And Tamil

Current Address : No:30, 4th Cross, Vigneshwara Nagar, Sunkadakatte - 560091 Bangalore, Karnataka.

DECLARATION:

I hereby declare that the above information furnished is true to the best of my knowledge and belief. Date : Yours Truly

Place : (KOTEESWARAN M)

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