SUMMARY
Senior Software Engineer with extensive experience with Hardware Design, and Software Design.
Designed Aircraft Engine Instruments Sets and Air data computers to airframe specification, full software development cycle and support for FAA certification.
RTCA DO-178B: familiar with all process including planning, requirements, design, coding, integration, verification, traceability, software problem report, software change request, and configuration management.
RTCA DO-160D: familiar with Environmental Conditions and Test Procedures: Temperature, Altitude, Vibration, Humidity, EMI, RF, and Lightning.
Languages: Over 15 years designing embedded C and 7 years embedded ADA.
PROFESSIONAL EXPERIENCE
DRS RSTA INC, Melbourne, FL
Software Engineer, Software Analyst
Analyzed Multitasking OOP ADA code embedded in Laser Guided Missile Target System. This was a multithreaded system, event driven, rendezvous, mailboxes, interrupts, and shared memory.
Wrote Visual Basic and National Instruments LabView source code embedded in Automatic Test Stations for Horizontal Technology Integration (HTI), Second Generation Forward Looking Infrared (FLIR), Thermal Weapon Sight (TWS), Driver’s Vision Enhancer (DVE), and Mass Mounted Sights system (MMS).
DUKES INC., Northridge, CA
Contractor Software Engineer
Designed the software and hardware for a Cabin Pressure Controller System. The software was developed in embedded C. The software development cycle was according to RTCA DO-178B. The Hardware of the Cabin Pressure System was tested according to RTCA-DO-160D.
Smiths Industries, Malvern, PA
Software Manager
Managed resources to successfully complete software design of Engine Instruments Display Set on the JPATS Program.
KOLLSMAN INC., Merrimack, NH
Electrical Engineer
Designed hardware with embedded software for Air Data Computers, Airspeed, Altimeter, Mach, Altitude Alerter, and Cabin Pressure Controller for various Corporate Jets Aircraft.
Designed a complete set of 6 engine instruments for the Piaggio Avante P180. The set included: Tachometer, Engine Temperature, Oil Pressure, Oil temperature, Fuel Quantity, and Engine Pressure Ratio.
Designed a Fuel Flow Indicator for the Boeing 727 and Boeing 737. This new instrument saved UPS thousands of dollars in fuel consumption.
The software cycle was developed according to RTCA DO-178B and the hardware was tested according to RTCA-DO-160D.
Quadrant Aerospace, Amherst, NH
Contractor Software Engineer
Developed software for C-130 Simulator Display Panel
EDUCATION
BS - Computer Science, Rivier College Nashua, NH: Jan-90, May-95
BS - Electrical Engineering, City College New York City, NY: 09-1975, 06-1980
TECHNICAL ADDENDUM
Languages: ADA, ANSI-C, C++, PASCAL, COBOL, Visual Basic, Assembly, National Instruments Lab Windows, Fortran, ABEL, SQL, Unix, HTML, Java Script, PHP, UML Fundamental.
Tools: Code Composer, Rational ClearCase, Software Configuration manager (PVCS), Requirement & Traceability Manager (RTM)., Razor, Microsoft Office, TI Tartan ADA compiler, DDCI Score ADA Compiler, MPLAB IDE, Nohau Emulator. Multimeter, Oscilloscope, Power supply, and Logic Analyzer,
Cadence Orcad Schematic Capture, Protel.
Regulations: FAA TSO, RTCA DO-160, RTCA DO-178B, MIL-STD-498, SEI CMM/CMMI.
Embedded Targets: Motorola 68HC11, 68332, Microchip PICxxx, Intel 8051, TI-TMS320.
Interface: MIL-STD-1553, Arinc-407, Arinc-575, Arinc-429, Manchester Code, ICAO Code, GPIB-488, Tachometer generator, Thermocouple, Eldec & GE Flow meters, Synchro Transmitter/Receiver, AC/DC Motors, Stepper Motors, , RS-232, RS422, LED & LCD displays, A/D, D/A, FPGA.
Aircraft Application: Learjet 35/36 & 50/55, Gulfstream II & III, Westwind 1124, Diamond IA & II, Citation III, Falcon 10 & 20, Beech Starship, Piaggio Avante P180, DC-8, DC-9, DC-10, Boeing 727 & 737, PT-6A Texan II (JPATS).
Engine Instruments: Tachometers (RPM, N1, N2), Engine Temperature (ITT, TGT, EGT), Engine Pressure Ratio (EPR), Fuel Flow/Fuel Used, Fuel Quantity, Oil Pressure, Oil Temperature, Torque Indicator.
Air Data: RVSM Altimeter Altitude Alerter, Air Speed, MACH, Vertical Speed (VSI) with TCAS, Air Data Computer, True Air Speed (TAS), Static Air Temp (SAT), Cabin Pressure System, 3ATI Horizontal Situation Indicator (HSI).