Avionics System Engineer

1. SWAMINATHAN BALARAMAN
BE, MS (By Research), AVIONICS, M I T
L&T SOUTH CITY APARTMENTS, BANGALORE – 560 076
Phone:+91 9731864926, +919738889292
beswaminathan[at]yahoo[dot]co[dot]uk
beswaminathan[at]gmail[dot]com
D.O.B: 04-September-1981
Skype: beswaminathan
Linked in profile: i n .li n ke d in .co m /in /ae ro sa mi
APM @ HCL Tech Project: Rockwell Collins (GNSS), CRANE
 Task Scheduling, Training, Review and monitoring of deliverables (SW Test cases).
 Conducting CAPA (Causal Analysis & Preventive Action) and Requirements Impact analysis.
 Risk identification and mitigations plan in compliant to PMP document.
 Coordinating with SQA for DO-178C compliance.
 As a Trainer (on demand) in Organisational Technical Training activities.
 As QA for CRANE EC-225 project, managing SY Verification, SW Development & SW Verification.
 Conducted Gap Analysis, Identifying Process Non-compliance (CMMi) and Risk Management.
♦ Working as Associate Project Manager (Technical) since April 2015, HCLT – Bangalore.
PM @ Sii ITeS (start-up) Project: Airbus FMS–SESAR – i4D Trajectory & eFFU
 Co-authored Initial 4D Trajectory A429 message structure derived from A702A-3.
 Analysed SESAR system requirements (SSS), System Safety Assessment (SSA/ARP4761), updated
the SA-LR ICD (SER) and resolved the same with suppliers (Honeywell, Thales and Saffran).
 Worked in Airbus SER ICD for EIS, i4D Trajectory & ATSU with Sii Toulouse, France (Onsite).
 Prepared Flight Test Request (FTR) for MCDU-R (ATA 22-82) for multiple power sources.
 Performed Failure Condition Analysis and FMS design for SESAR project.
 As Business Analyst, secured the eFFu project from Sii France.
♦ Worked as a Project Manager (Technical) with SII India ITeS (start-up), Aug14 – Feb15.
TL @ Project: EMBRAER E2 Primary Flight Control Systems
 Engineering & Requirements Management for Primary and High Lift Flight Control Systems using
IBM DOORS tool complying with ARP4754 standard and reporting through Agile-Scrum process.
 Involved in Development of primary Flight Control System Internal-ICD (A429 & CBDL)
 Involved in review of Embraer E2 Wiring diagram for Primaries, Spoilers and FCC
 Involved in actuator, inceptor allocation and CBDL internal linking at different levels.
 Involved in PDR activities for Moog Inc, NY, USA (onsite)
♦ Worked as Technical Lead for Flight Control System(Embraer) and Project Manager for handling
EMBR E2 Iron Bird Requirements in Moog India Technology Centre, May2013 to Aug2014
Other Responsibilities:
 As DOORS admin for Moog India, new project configuration and access control.
INNOVATION
Ideas submitted
 Swift Operation of Engine Thrust Reverser in Passenger Aircraft
 Requirements and workflow for Requirements Management Tool -
Automation
Specialist@ Project: Renault Nissan – Engine Management Systems – CMF1
 Analysed Diagnostic Fault Codes for OEM and RB layers for Renault Nissan CMF1 project
 Designed, developed & validated an automation tool that differentiate automatically the
functional changes in system SW and received the award from Department Head.
 Released the System Specific Data (SSD) for the project and conducted IO tests in HIL loop.
 Worked in implementation of Fuel Temperature Emulation (FTE)
 Worked in implementation of Pressure Limiting Injection (PLI) for Euro7
 Mentoring software team on different vehicle functions with know how and providing testing
strategy.
♦ Worked as a Specialist (equivalent to APM) in Robert Bosch(RBEI), June2011-May2013
Cross Functional Activities:
 Worked as a competency development manager in department level covering 140+associates.
Planned, scheduled and executed training plans.

2. INNOVATION
Ideas submitted
in BOSCH
 Multi axis fuel injector
 Improving fuel efficiency in IC engine by optimal use of operating
parameters
 Methods of varying engine displacement for reciprocating engines.
 Static Fuel quality detection – concept
 Drunken driving deduction
 Improving passenger safety during life threatening situation.
Did BE final year project at PRICOL Coimbatore on Automobile domain 2004 (Vehicle Payload Indicator)
Worked as a consultant for Compaq HP project in SGS, July 2004 - Jan 2006
Senior SWE – Cyient (Infotech) Airbus 400M – Load Master Control (LMC)
 Performed the System testing activity(Test Cases and Procedures) for Airbus400M LMWS module
 Executed the IOC test cases in Techsat ADS2 real time simulator (SIB) along with A400M Flight
hardware at AIRBUS, Germany (onsite).
 Analysed the MFD (Scade) requirements for IOC & SOC phase for civilian and military versions.
♦ Worked as a Senior Engineer in Infotech Enterprises (Cyient), September2009 – June2011
Senior Engineer - HTSL Project: Airbus Flight Management Systems
 Analyzed & Verified System requirements for Airbus A380 PERF module in FMS (SRD).
 Worked on A380 MFD initial development tasks (SER) and PDB Robustness update.
 Software design & development (SDD & SRC) for Speed Change prediction and display in ND.
 Involved in system level fault analysis & reporting for A380 FMS.
Certification: Six sigma Greenbelt, July 2009
Self-Learnings:
 General awareness on Airbus Civil aircraft series of cockpit systems and flight operations briefing.
 General awareness on Airbus FCOM for ATA 22 and ABD100
♦ Worked as a Senior Engineer in Honeywell Madurai, June08 – Aug09 (after submitting MS thesis)
INNOVATION
- ideas worked out
at Honeywell 2008
 FMS - Auto derate function, Avoiding Aircraft landing Accidents (ALA) & Projector less
HUD
 Power Steering in fighter jets
 Deep Space Network – Honeywell Technical Symposium 2008
Project Associate - CASR Project: ANUSAT – Satellite Attitude Control System
 Project in collaboration with CASR (MIT) & ISRO Satellite centre, Bangalore. Launch year 2009
 Developed the Software Requirement Specifications Document (SRS)
 Validated control algorithms for stabilizing Micro satellite for the modules spin axis orientation
towards normal to the sun vector, which is implemented first time in Indian satellites.
 Work done for Closed Loop Testing (HIL) interfacing magnetometer and sun sensor.
 Developed Ground Procedures to recover the spacecraft Attitude during contingency
♦ Worked as a Project Associate, MICSAT CASR, MIT Chrompet, Chennai, May 2006 - May2008
MS Research Project SPACE MISSION ANALYSIS AND DESIGN FOR TACTICAL SPACECRAFT
 Spacecraft Attitude Control System supports both spin stabilized as well as 3 axes stabilisation
 Mission analysis for Flight Dynamics and Attitude control simulated using COTS software
♦ This research was undertaken for MS (By Research) thesis, while working as Project Associate at
MICSAT CASR, MIT Chrompet, Chennai – Feb 2006 to June2008. Graduated in Feb 2010.
Publications Research work carried out at MIT is published in the following conferences
Paper 1 Space Mission Analysis & Design for Tactical Spacecrafts
Paper 2 Magnetic Attitude Control for a Spinning Spacecraft with Cross Product of Inertia
Conference IEEE AIAA Aerospace International Conference, USA, March 7-14, 2009
Paper 3 Closed Hardware in loop real time attitude control simulator for a Spinning Spacecraft
Conference National Conference on Instrumentation & Control -ICECON 07, NIT Trichy, 2007
CV - Version: 1.61 2

3. ACADEMIC
CREDENTIAL
CV - Version: 1.61 3
* 2000-2004 Shanmugha College Of Engineering (now SASTRA) affiliated to Bharathidasan University
B.E in Electronics and Instrumentation Engineering – Full time
REFERENCE Mr. S.Gurudev, (Former Group Director ADE)
Section Head, FTE
Moog India Technology Center (MITC)
guru10122003[at]yahoo.co.in
Mr. Rajesh Chaubey / Mr. Ravi Holla
Project Lead, iFMCNS – Platforms & PERF,
Honeywell Technological Solutions Lab,
Rajesh.Chaubey[at]honeywell[dot]com
Mr. Srihari Jayathirtha,
Project Lead, iFMCNS,
Honeywell Technological Solutions Lab,
Srihari.Jayathirtha[at]honeywell[dot]com
Mr. Niranjan Mariyanna,
Senior Expert, ECW - ECU System Dev,
Robert Bosch Engineering and
Business Solutions Limited (RBEI/ECW)
Niranjan.Mariyanna[at]in[dot]bosch[dot]com
* 2006-2010 Madras Institute of Technology [MIT], Anna University, Chennai
MS (By Research) in Avionics (Aviation Electronics) – Full Time
Research Space Mission Analysis & Design for Tactical Spacecraft