V. Rathinakumar is seeking a position that allows him to fully utilize his skills and contribute to personal and corporate goals. He currently works as an engineer at CSIR - National Aerospace Laboratories in Bangalore. In this role, he has modeled various systems for the SARAS aircraft in MATLAB Simulink, including the stall warning system, pitch trim actuator and warning system, and autopilot mode transition logic. He is responsible for verification and validation testing, hardware and software integration testing, design work, and document review. Rathinakumar has an M.Tech in Aerospace Engineering from IIT Madras and a B.E. in Aeronautical Engineering. He has expertise in MATLAB Simulink

1. V.RATHINAKUMAR
71-HANUMAN NAGER, NEW THIPASANTRA ROAD,
HAL 3RD STAGE, BANGALORE, MOBILE NO: +919003435955
PIN CODE-560075. EMAIL ID: rathina2020@gmail.com
OBJECTIVE
To serve the company to my fullest capabilities, taking up challenging assignments, enhancing
interpersonal skills, sincerity and team spirit at work place that would lead to the fulfillment of
personal and corporate goals and to strive for the growth of the company.
CAREER SUMMARY
ORGANAISATION:CSIR - NATIONALAEROSPACE LABORATORIES,GOVT. OFINDIA
PLACE-Bangalore
POSITION-Engineer
JOINEDON-7th OCT2014 – Present Day
TECHNICAL EXPERIENCE
PROJECT DESCRIPTION
1. TheSARAS aircraftbeing designed and developedby CSIR NAL is equipped withStall warning
system which is responsible for alerting the aircraft crew about stall condition. The system
also provides the Landing, Takeoff, Hydraulic low pressure, Pitch trim and over-speed
warnings. The application software is designed as per the RTCA DO178B Level A standards.
2. Designed the SARAS AircraftPitchTrimMechanicalSetup and analysis is taken care,Software
algorithms of pitch trim setup is imported in the designed Simulink model, test cases of the
pitch trim setup is verifiedwith the Simulink model and VCP test cases are verified, warning
algorithm of pitch trim is imported in the model and test report has generated automatically
and its verified with original Aircraftpitch trim setup.
3. The SARAS Aircraft Autopilot and Mode Transition Logic (MTL) being designed by using
Matlab State flow Approach. The test cases of MTL is verified with this Simulink model and
Automatic test cases are generated. Using Simulink design verifierthe modelwas verifiedand
the Automatic Code generation was generated the Embedded C code. This Auto code is
verified withthe source code got the 100% of accuracy.
4. The Auto code of MTL is compared with RTRT. Comparison is 100% true and this Auto code
can be used as source code in the stall warning system.

2. ROLE-DESIGN TEAM
 Modelled Stall Warning System of SARAS Aircraft in Matlab Simulink tool.
 Modelled PitchTrim Actuator Response and PitchTrim Warning System in Simulink.
 Modelled the SARAS Auto Pilot MTL in Matlab State flow Approach.
RESPONSIBILITY
 Verification and Validation
 SWS/AIC Rig testing
 Execution of the HSI test on the avionics test rig.
 Test Report generation.
 Hardware/ SoftwareIntegration Testing
 Review of HSI VCP along withchecklist generation.
 Test execution & Report generation.
 Problem report generation.
 Dynamic analyses of complex algorithms using Matlab Simulink 2013a.
 Validation of verification cases and procedures (VCPs) using model based approach
(Simulink).
 Design
 Designed Stall Warning algorithm as per AIC (aircraftinterface computer).
 Designed PitchTrim controland warning algorithm.
 Designed Pitch Trim model using Simulink and performed dynamic analysis for
various inputs and analyzed the generated warning algorithms
 Designed SARAS Auto pilot MTL and test report was generated.
 Document review
 Reviewed the requirements and the design documents: SRS (System Requirements
Specification), SWDD (Software Design Document), SRD (Software Requirements
Description), and SDD (System Design Document). Checklist generated. Problem
report generated
ACADAMIC DETAILS
M.tech Aerospace Engineering IITMadras 2013 CGPA-7
B.E Aeronautical Engineering Anna University Chennai 2010 67%
HSC State Board 2006 75%
SSLC State board 2004 87%
COMPUTER SKILLS
o Operating system : WindowsXP onwards & Linux Ubuntu
o Basic skills : MS office,latex
o Programing skills
Expert: Mat lab Simulink 2012 onwards, RTRT,C, Catia V5
Average: AutoCAD, ProE
EXTRA CURRICULAR ACTIVITIES
o Won 1st prize in water rocketry national level competition at Kruksatra Anna University
2009.

3. o Won 1st prize in Glider national level competition at MIT Chennai 2008.
o Won 1st prize in Water rocketry national level competition at Nehru college of Engineering
Coimbatore 2009.
o Won2nd prize in hydrolauncher national level competitionat VSB Engineering College Karur
2010.
o Won consolation prize in Glider national level competition GCT Coimbatore 2008.
o Participated UAV national level science Exhibition at VSB Engineering College 2010.
o Participated ETAAero modeling at Vel Tech College Chennai 2009.
o Participated in Futura Projectdesign national level science Exhibition at BIT 2009.
o Participated in Scontra paper presentation and Aero modeling at REC Chennai 2008.
PUPLICATION
 IEEE -2015 2nd International Conference on Computing for Sustainable Global Development
Title-Validating VCP using Model Based Approach
Copy Right INDIACom-2015: ISSN 0973-7529; ISBN 978-93-80544-14-4
 Title-Effectof Voltagevariation in Electrodytrodynamic (EHD) pump
JOURNAL NAME-International Journal of Emerging Technology and Advanced Engineering
IJETAE,Volume 5, issue 7, July 2015.
PERSONALDETAILS
Date of Birth : 29/October/1987
Nationality : Indian
Marital Status : Single
Gender : Male
Languages known : English, Tamil
DECLARATION
I do hereby declare that the particulars of information and facts stated herein above are true,
correctand complete to the best of my knowledge and belief
Date: Signature
Place: (V.RATHINAKUMAR)