System Data
Resume:
Chethan Kumar M
*th 'C' Main, RPC Layout, E-mail:
**********.***@*****.***
Vijayanagar, Bangalore -104 Mobile No: +91-
Career Objective
A technocrat with over 2.1 years of experience in software
development, verification, validation & System testing in Electronics and
embedded Avionics Weapon Systems of military aircraft, seeking a
challenging career in an esteemed organization, which harbors talent,
encourages innovation and promotes professional growth.
Profile Summary
> Intensively worked on design, development & Testing of Avionics Projects.
> Extensively worked on HSI, SI & Unit Testing.
> Testing of Avionics Systems in the Integrated Environment like Avionics
Integration RIG.
> Generated Software Requirement Specification (SRS) for SSCDRMK-II GRE as
a part of SDLC.
> Requirement analysis and system level verification of Avionics Mission
computer (OAC) at RIG Level with subsystems in integration platform.
> Generated Test plans, Test Cases and Test procedure documents for various
avionics LRU functional testing at Avionics Integration Rig with
integrated systems.
> Focused on Organizational Goal & capable of planning and implementing
projects
Professional Qualification
. M.Tech (VLSI & Embedded System) from SSIT, Tumkur with 84.3% in 2014.
. B.Tech (E.C.E) from APS, VTU, Belgaum with 65.66% in 2010.
. Intermediate (10+2) from BVVS INDP PU College, Harapanahalli with 71.66%
in 2006.
. 10th from TVS, Huvinahadagali with 89.28% in 2004.
Technical Skills
. Languages : C, Embedded C, Verilog HDL
. Operating Systems : Windows XP/7, Linux
. Development Tools : MATLAB (Simulink, Guide), Xlinx ISE 13.2, MVC++
6.0, Keil uVision4
. Testing Tools : Various in House (PATS, PASIT), Modelsim 6.3f.
. Standards/ Protocols : Mil-Std-1553B, DO-178B, RS232, RS422,CAN
. Microcontroller : Basics of 8051, ARM7-CORTEXM3
Professional Experience Track Records
Project 1: System Integration, Verification, Analysis & Tools
Development for Functional Testing
Role : Integration, Verification, Analysis and Test
Report generation
Programming/ Tools : C, Mat-Lab (Guide), MVC++ 6.0 GUI (MFC), MS-Office
(Excel)
Platform : Windows XP
Hardware Used : PCMCIA Two Node 1553 Condor card for Laptop
PCMCIA RS 485 Two Port
National Instruments Card
Protocol : MIL-STD-1553B, RS422
Synopsis : Avionics Integration Rig (AIR) is an integrated
environment designed for testing of mission/safety critical subsystems
(LRUs) of Light Combat Aircraft (LCA). Extensive Hardwire-In-Loop
Simulation (HILS) and Testing of LRUs concerning to Avionics & Weapon
System (AWS) needs to be carried out in order to reduce the time and cost
associated with real flight-testing. Preparation of test plans and
procedures for validating system behaviour is the prerequisite of
testing. Proper functionality of Mission Computer (OAC) with other LRUs
connected to it through data bus and/or discrete lines as well as Cockpit
Displays with mode selection through switches have to be ensured before
its aircraft installation and flight test.
Contribution :
Tools Development:-
. Developing Post Flight Data Analyser that automatically searches
the required parameters from Video/Flight Digital Recorder
(VDR/FDR) files and represents navigational parameters graphically
and generates performance report.
. Designed Diagnosis Tool for off-line checking of mode status words
of all avionics LRUs. It is to be used by ground engineers for
flight clearance. GUI front-end is designed using VC++ and database
is managed in MS Access.
Verification & Analysis:-
. Analysis, verification and validation of different functions from
Control/Display units of Flight Management System (FMS) like Flight
Plan, Basic Flight Steering, Auto Navigation, Speed Guidance and
Approach and Landing Guidance, Flight Envelope Monitor from Primary
and Secondary Flight Control System information, Management of
Aircraft Systems (Engine, Fuel, etc) and warning Management.
. Verified different display symbologies on Multi-Function-Colour-
Display (MFD) for radio Navaids like VOR/ILS and TACAN.
. Unit Level Testing performed on SSCDRMK-II Application Code during
design stage.
Others:-
. Verifying the wiring diagram, wiring matrix, wiring harness and
signal conditions before installing new LRUs in integrated
environment.
. Integrated rear cockpit for trainer version of LCA and validated
switch and display control logics for front as well as rear
cockpit.
. Perform the Solid State Crash Data Recorder (SSCDR) system
integration testing for production clearance with sub systems.
Project 2: - SSCDRMK-II for LCA-Tejas
Role : Developer and Tester
Client : Indian Air Force (IAF), Indian Navy
Programming/Tools : C, MVC++ 6.0, MS-Office (Excel)
Operating System : Windows XP
Database : MS-Access
Emulator/Debugger : Vision Click, USB ICE for ADSP 21060
Description : SSCDR MKII is an upgrade of previous SSCDR
MKI. Upgrade is done to overcome limitations of previous system. It
acquires sensor data (analogue, discrete & frequency) data from flight
control system (FCS) through RS 422 interface and digital data on MIL
1553 Bus. It also acquires one channel audio data. It stores the acquired
data to a crash protected memory module. It has Ethernet & RS 422 (back
up interface) for milking out the recorded data.
Responsibility :
. Hardware Software Integration & System Testing with Test Rig which
simulates A/c signals.
. Interaction with clearance agencies for airworthiness certificate.
. Coding (Lower Level Classes) & target testing.
. Data retrieval from SSCDRMK-II LRU after post activity for Testing.
. Generation of Test Plans, Test Cases and Test Procedures documents
for SSCDRMK-II GRE.
Personal Profile
Father's Name : Chethan Kumar M
Date of Birth : 16 OCT 1988
Languages Known : English, Hindi, Kannada, Telugu, Tamil
Nationality/ Sex / Marital : Indian/ Male/ Single
Status
Passport : Applied
Permanent Address : S/o Chandranna M, Near Bus Depot,
Hoovinahadagali(Tq),
Bellary,Karnataka-583219
References
Will be presented on request
Date:
Place: Bangalore
(Chethan Kumar M)
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