Software Engineer Senior

Curriculum Vitae

Ashwini.V.Kamshetty Email: *******.****@*****.***

****, *** **** ****, ***, Oak park,

California 91377

Phone: 747-***-****

Total Experience

* *** * *****

Previous Designation Held

Senior Software Engineer

Professional Snapshot:

A dynamic, skilled, performance driven IT professional with experience in Verification and Validation of Real Time Embedded Avionics Application Systems.

Acquired onsite (Germany) work experience in design and development of one of the military aircrafts.

Experience in Verification and Validation in compliance with DO-178B standard.

Hands on experience in various methodologies and processes, knowledge of complete SDLC. Strong in Technical Documentations.

Excellent client interaction skills with global end customers in getting requirement clarifications and delivering work on time.

Provided technical training sessions for the freshers in the company and expertise in giving professional presentations.

Strong ability to give constructive criticism for peer's work during review.

Flexible, mobile and willing to go on an assignment on short notice.

Ability to take challenges, Passion to Learn, Share and Implement new technologies, Work under pressure and independently contribute towards project completion at any layer of project execution.

Educational Qualification:

Bachelor's Degree in Computer Science & Engineering, 2005 Passed out with 71.5%, from P.D.A College of Engg, Gulbarga, affiliated to Visveswaraiah Technical University (VTU) Belgaum.

PUC from Smt.V.G. Women’s College, Gulbarga, in 2001, with 60.5%.

SSLC from St. Joseph’s Convent School Gulbarga, in 1999 with 85.6%.

Technical Expertise:

Operating Systems

Programming Languages

Defence Standards

Design & Test Tools

Configuration Management Tool

Requirement management Tool

Software Packages

Exposure to

Linux, VxWorks(RTOS),MS-Windows Vista\XP\7

C, exposure to Ada95

DO178B & DOD-2167A

Artisan, Rhapsody 6.1, Cygwin RTRT, AdaTest95,Eclipse.

Visual Source Safe, Clear Case, SVN, CM

Synergy,

DOORS

Beyond Compare, Understand C, GNAT style checker

UML.

Professional Exposure:

Was working for Infotech Enterprises Ltd(CYIENT), for their embedded solutions in avionics. (Oct 2008 to March 2014).

Served for Silver Atena Pvt. Ltd (Feb 2007 to Oct 2008).

Worked in Aeronautical Development Establishment (A.D.E Defence R & D Organization) (Feb-2006 to Feb-2007).

Projects:

Project : Liquid Pump Motor Controller -787-9

Organization: Infotech Enterprises Limited (ACE Certified Silver Medal Company)

Client : Hamilton Sundstrand, US

Duration : April 2012 – Jan 2013

Software used : SITE, C, Eclipse, SVN, Cygwin, pathfinder Safety Integrity Level : DO-178B, Level B.

Project Brief:

Each LPMC is a motor control Inverter comprised of an input filter, output filter, power inverter, and a control board consisting of PPC and DSP microprocessor. Its primary function is to convert 230VAC input power to three-phase AC output power to drive the attached motor, which in turn controls the electrically driven liquid pump. The output voltage and frequency are varied in such a manner as to control the torque and speed of the motor as it performs associated motor functions. The LPMCs protect against wiring faults and provide other protection functions (e.g. over-speed, DC link over voltage, ground fault interrupt, over temperature). The protection functions provided are dependent upon operating mode.

The LPMC communications link to send/receive system information to/from the aircraft is via a Controller Area Network (CAN) bus. The CAN bus integrates with the aircraft Common Computing System via a Remote Data Concentrator. The LPMC communicates with the Pack Control Unit. The CAN bus sends and receives control commands and status messages including speed command, speed feedback, motor temperature, and maintenance data.

My Role:

Involved in design and development of test case and test procedures for high level requirements.

Development of .java test script that is run on client server test environment (SIT) for software integration testing .

Understanding of hardware software integration of PPC-555 test rig to execute test procedures and test result preparation.

Prepared Formal Review Work Instructions based on HS SWSPs.

Performed peer and formal Reviews.

Gave training on various HS SWSPs, testing methodologies and work instructions.

Project : 3G Core Analysis

Organization : Infotech Enterprises Limited

Client : Hamilton Sundstrand, US

Duration : May 2010 – April 2011 Software used : SITE, C, Eclipse.

Safety Integrity Level : DO-178B Level A.

Project Brief:

The Third Generation SPDA is an Integrated Modular Avionics (IMA) product. The Product provides Secondary Power Management and Distribution allowing for application specific utility management functions for the target airframe application My Role:

Involved in Test Case Development.

Involved in Peer Reviews of Test Scripts.

Analysis along with review of High level and Low level Requirements. Involved in Regression Testing.

Project : A400M

Organization : Infotech Enterprises Limited(CMMI level 5 Company)

Client : Airbus, Germany

Duration : October 2008 – April 2010

Software used : Artisan Design tool, DOORS, Clear Case.

Safety Integrity Level : DO-178B Level A.

Project Brief:

The Airbus A400M is a four-engine military transport and tanker. It provides excellent field capabilities and requires only a short runaway length, both for take-off and landing. As a tactical airlifter, the A400M is capable of air dropping paratroops and equipment via parachute or gravity extraction. It can drop simultaneously paratroops & cargo. The A400M is also quickly convertible into a tactical tanker to refuel a wide range of aircraft and helicopters.

My Role:

Cross verification of the SRDs.

As part of the design team in Germany I created the design for Waste Water System, Anti Noise and Vibration System, Guide and Restrain Control.

PR fixing and updation.

Design reviews.

Project : LGERS V&V

Organization : Silver Atena (CMMI level 5 Company)

Client : Airbus

Duration : Feb 2006 – May 2006

Software used : RTRT using Green Hills compiler, C language Safety Integrity Level : DO-178B Level C.

Project Brief: Landing Gear Extension and Retraction System (LGERS) Control

Software, installed on Central Processor Input Output Modules (CPIOM) within the A380 Integrated Modular Avionics (IMA) system. LGERS contains software COM with [DO178B] Level A and S-BITE with [DO178B] Level C criticality. The verification activity covers Code scrutiny and Module Testing.

My Role:

Responsible for the Code Review of the modules against the module design specifications. Re-reviews of the code modules following rework by GE Aviation for review comments

Develop the Test Script.

Requirement based Module Test Review.

Generate & review test specifications. Execution of test cases on target

Project : FQMS (Fuel Quantity Management System)

Organization : Silver Atena

Client : Goodrich

Duration : 8months

Software used : RTRT using Green Hills compiler,ADA language Safety Integrity Level : DO-178B Level C.

Project Brief:

This software is developed for BOEING 787 aircraft and developed using Ada 95 . The purpose of this software is to measure the fuel quantity in each tank and provide outputs of this data and total fuel, on the ARINC 664 compliant Common Data Network (CDN) interface.

My Role:

Qualification tests for C, using RTRT tool on the target board TMS 2812.

Qualification tests for Object-Ada, using RTRT tool on target board MPC565.

Traceability of test case document using doors.

Module Testing.

Project : CADS(Controlled Aerial Delivery System)

Organization : DRDO

Duration : Feb 2006 up to Feb 2007

Software used : Rhapsody, Adatest95, Ada Safety Integrity Level : DOD-2167A Project Brief:

CADS is based on the Ram Air Parachute (RAP) system designed to deliver a 500kg payload to a designated point within a 100m Circular Error Probability (CEP). Within the energy limitations, the CADS, with this AG&CS automatically steers itself to designated point by operating the two lanyards as a function of the cross-track error in the flight path and heading errors etc. The control inputs to the PFCC are provided by Global

Positioning System (GPS) receiver, Magnetic heading sensor, Altitude Sensor, Hand held

Terminal, Ground Control System (GCS) through RS232 link. Data Recording Unit (DRU) also functions as Encoder/Decoder (ED). The PFCC control outputs include port and starboard lanyard actuation, RS232 serial data link for DRU and GCS.

My Role:

Design of CADS using Rhapsody

Testing

Software Configuration Management

Personal Profile:

Name

: Ashwini Kamshetty

Gender

: Female

Linguistic Abilities

: To speak, read and write-Kannada, English & Hindi.

Hobbies

: Reading Books, Travelling, Playing Badminton & Chess.

Declaration:

I hereby declare that the particulars given herein are true to the best of my knowledge and belief.

Place : Bengaluru. Ashwini Kamshetty

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