Areas of

Expertise:

. Open System Architectures, Object Oriented Analysis and Design;

. Requirements Development and Management using DOORS;

. CCSDS Telemetry and Real time Avionics Data Acquisition and Monitoring

Systems

. System Simulation and Modeling

. Inertial Navigation Systems;

. Cockpit Displays & Controls

. Integrated Diagnostics & Prognostics Test systems, Fault Tolerant/Safety

Critical Systems;

. TCP/IP and Network Protocol Stacks,

. MIL-STD-1553B, FDDI, LAN/WAN,

. ARINC-429, CAN,

. AN/ALQ-161 EW

. EO/IR Sensor

. SCM using Rational ClearCase/ ClearQuest;

. CMM Level 4 practices

. DO-178B

. UML

Languages:

. C/C++,

. JAVA,

. Ada,

. Perl,

. SQL

. 1750A assembly

. C#

Operating Systems / Processors:

. VxWorks

. SUN Solaris

. SGI Irix

. Windows 2000

. PowerPC

. M68040

. MPC551x

. PIC and ARM microcontrollers.

Tools:

. Green Hills AdaMULTI

. Wind Rivers Tornado IDE

. Visual Development Studio

. MS Project

. Oracle

. MS Access Database

. Rational ClearCase and ClearQuest.

1

Actively seeking a position as a

- Software Engineer Financial Systems -

with a reputable organization in need of a professional with uncompromising

milieu in different key positions such as Software Systems Engineer, Senior

Software Engineer, Senior Computer Systems Specialist, Staff

Engineer/Consultant, Research Scientist, and specialization in programming

and systems integration; with solid experience that will benefit from

initiative, organizational skills, hard work ethics, multi-tasking

abilities, and drive to exceed corporate objectives.

Dynamic, highly motivated and goal-oriented professional with several years

of unyielding experience in different companies in key positions as

Software Systems Engineer, Senior Software Engineer, Senior Computer

Systems Specialist, Staff Engineer /Consultant, Research Scientist.

Software Systems Engineer with experience in design, development and

integration of real-time embedded systems for airborne and space

applications. Solid background in programming, systems integration,

verification & validation with demonstrated technical leadership.

Excellent verbal and written communication skills. Pro-active, self-starter

who is able to multi-task in a fast paced environment while helping produce

high quality work.

Key Skills

> Experienced in all phases of software development life cycle management

from conceptual design to delivery

> Configuration management and deployment of operational and test

software releases, including system integration testing, verification,

and validation

> Achieved significant cost savings by streamlining system development

plans and processes on a number of programs

Professional Experiences

Medtronic MiniMed E Northridge, Ca

8/2009-4/2010

Principal Software Engineer (Consultant), External Pump R&D

< Developed test plan/procedures and supported software integration

testing of the Patch Delivery System (PDS) that provides comprehensive

diabetic disease management solution. C#, .NET environment, Windows CE.

Controller and Pump devices associated using wireless RF communications

in a WPAN.

< Reviewed product and subsystem software requirement specifications for

agile planning of sprint releases of key product features and risk

mitigation.

< Used Test Track system to document system integration problems and aid

developers in resolving software issues.

MEGGITT SAFETY SYSTEMS INC E Simi Valley, Ca

4/2008-6/2009

Sr. Software Systems Engineer, Systems Engineering Department

< Reviewed Boeing 777F Cargo Smoke Detection System (CSDS) Specification,

Equipment Specifications, and Software Requirements Document for

requirements coverage and flow-down from customer specification to

actual design and verification.

< Developed Supplier Specification and Software Requirements for the

Learjet LJ-200 Fire Detection and Extinguishing System. Used

Requirements Management tool, DOORS.

< Developed Interface Definition Document, System Description Document and

PSAC documents for the FIDEX system to satisfy requirements of DO-178B,

Level B.

< Achieved significant cost savings by streamlining system development

plans and processes.

NORTHROP GRUMMAN Electronic Systems E Azusa, CA

9/2002-4/2008

Senior Systems Engineer, SBIRS System Engineering Integration & Test

< Contributed to the overall development of SBIRS HEO ground architecture

and Concept of Operations.

< Developed Software Requirements Specification (SRS) for SPOTS Executive,

a key component of SBIRS HEO Satellite Payload Orbital Test Station

(SPOTS) software infrastructure.

< Lead responsible for SPOTS Executive software development - a network-

distributed client/server model that provides software infrastructure

for SPOTS - Java, C/C++, CORBA and Oracle database.

< Designed CCSDS telemetry display pages for Satellite Payload Diagnostics

System (SPDS) integrated with off-the-shelf EPOCH Telemetry Tracking &

Command (TT&C) software package to provide real-time state-of-health

monitoring of Payload.

< Developed capability to monitor the State-of-Health, availability of

resources in SPOTS Data Center consisting of distributed SGI, SUN and

Windows server/work stations to meet SLA goals.

< Responsible for Software Configuration Management for SPOTS software

running on SGI, SUN and Windows platforms using Rational ClearCase.

Developed and implemented software Build & Release management strategies

to facilitate timely product releases. Build System with over 200

Makefiles.

< Supported Operational deployment of software releases including system

integration testing and verification and validation of requirements and

change/discrepancy resolution.

TEKELEC CORPORATION E Calabasas, CA

2000-2002

Senior Software Engineer

< Responsible for product design reviews and development strategies for

continuous product development for Message Generator and Traffic

Simulation (MGTS) system. Developed command line interface software to

test SS7 links. Familiar with UTMS and 3G protocols. C/C++, SUN Solaris.

LOCKHEED MARTIN SKUNK WORKS E Palmdale, CA

1997-2000

Senior Computer Systems Specialist

< Principal investigator for IR&D responsible for design and development

of common, reusable Modular Avionics Architectural (MAA) framework for

use across various tactical fighter aircraft platforms. Successfully

prototyped and demonstrated the proof-of-concept, plug and play

capability of different software and hardware building blocks in support

of legacy avionics upgrades. Open, Scalable and COTS based solution.

Demonstrated cost savings of over 40%.

< Developed Models for INU, ADC, RALT and Cockpit Head-Down-Display Object

Models. Integrated three (3) different vendor solutions for cockpit

multi-function displays to demonstrate plug-and-play capability of MAA.

VME MC68040 and Power PC running VxWorks, 1553B and FDDI. Object

Oriented design utilizing C/C++, Green Hills AdaMULTI; Wind Rivers

Tornado IDE.

< Presented briefing on Lockheed's IR&D effort to the modular avionics

architecture subcommittee at the Society of Automotive Engineers (SAE),

April 1999, Nashville, Tennessee. Member of SAE ASD, AS-5 and AS-2

standards development subcommittees.

< Developed Advanced Affordable Avionics Architecture (A4) concept design

for next generation unmanned air vehicles (UAV) and a test bed for

evaluating technologies for highly reliable, autonomous control of UAVs.

Developed top-level architecture for Mission Systems, Communications

and Sensor Systems domains for a C4ISR platform. Presented design to

AFRL, Dayton, Ohio, May 2000

AIL SYSTEMS, INC E Lancaster, CA

1994-1997

Staff Engineer /Consultant

< Developed software to monitor six different MIL-STD-1553B avionics

system buses for the B-1B Avionics Data Acquisition and Control System

(ADACS). Used M68030, Ada and VxWorks in VME bus based flight

instrumentation system.

< Supported B-1B Block-C Flight Test Data Reduction/Analysis, FORTRAN.77,

DEC VMS. AN/ALQ-161 target identification & performance analysis.

Coordinated performance analysis with B1-B CTF personnel at Flight Test

Data Center, Edwards Air Force Base, California.

TELEDYNE SYSTEM COMPANY E Northridge, CA

1991-1994

Research Scientist, Army ASM Program (CCATD)

< Developed position/navigation subcapability for Army Vetronics

Automotive Test Rig (ATR) Drive-By-Wire System. Integrated Litton's LN-

100 INU into ATR Vetronics.

< Designed and developed integrated Diagnostics/Prognostics Test (IDPT)

for ATR, using Ada.

< Implemented memory error detection and correction (EDAC) diagnostics

software integrated into the MILSTAR Satellite processor's comprehensive

Perceptive Diagnostics (PD) CPCI.

< Updated PD CPCI Test Plan to establish requirement tractability and

coverage for FQT of deliverable software; telemetry data analysis and

review of overall PD CPCI design and Software Development Specification.

DOUGLAS AIRCRAFT COMPANY E Long Beach, CA

1989-1991

Principal Engineer/Scientist, C-17A Avionics Systems Engineering

< Group Leader responsible for the overall C-17A, Avionics Multiplex Data

Bus architecture development; interface control definition and data bus

requirements specification. Performed protocol scrub to ensure BC/RT

compatibility. Supported analysis of C-17A Cockpit Electronic Display

design.

< Performed analysis of data bus loading; Mission Computer (MC) throughput

utilization. Supported review of MC OFP software design with Air Force,

CPDS, CPPS, CPTPlan and CPTProc data items per DOD-STD-2167A.

< Coordinated Subsystem/System Level Testing and Integration of the

complete suite of C-17A avionics with hardware-in-the-loop using Flight

Hardware Simulator. Supported development of Avionics Integration Lab

Simulator using actual LRUs and MC OFP simulation.

TELEDYNE CONTROLS E West Los Angeles, CA

1986-1989

Senior Member of Technical Staff

< Lead Software Engineer responsible for the complete requirements

analysis system design and development of V-22 Osprey Vibration,

Structural Life and Engine Diagnostics (VSLED) system, MIL-STD-1679

development. Project Lead involved with all phases of product

development from concept to complete deliverable box. VMX RTOS kernel

running on 1750A Mission Processor working with two TI-320C25 DSPs;

10,000+ SLOC, JOVIAL.

LITTON GUIDANCE & CONTROL SYSTEMSE Woodland Hills, CA

1980-1986

Senior Engineer

< Software Engineer responsible for Built-In-Test Fault isolation software

for the F-15/E RLG based inertial Navigation Unit F-15 INU. Familiar

with Kalman Filtering & Inertial Navigation system principles.

< Group leader responsible for design and development of the LN-20

SIDS/GPS 1553B data Bus Controller, CDU and Flight Test instrument

interface unit software.

< Developed Software Checkout Console (SCC) that provided debug

capabilities for testing Flight Software for the various Inertial

Navigation Unit platforms.

Educational Background

M.S. Major: Computer Sciences

UNIVERSITY OF CINCINNATI + Cincinnati, Ohio

B.S.E.E. Major: Electronics and Communications Engineering

OSMANIA UNIVERSITY + Hyderabad, India

Contact this candidate