Experience

Avidyne

• United States
• Aviation and Aerospace Component Manufacturing
• 100 - 200 Employee

• Senior Software Engineer

  • Mar 2004 - Present

  Responsible for software development of integrated flight decks. Develop real-time embedded software for FAA-certified avionics equipment. Develop components of an integrated Flight Display System. Integrated flight deck for general aviation. Application lead for Aircraft Configuration Module (ACM), Front Panel Services Module (FPSM) and Multi-purpose Input/Output (MPIO). Application lead for Enhanced Vision System (EVS). Responsible for the development and certification of the EVS system. Integrated flight deck for Eclipse E500 Jet. Application lead for Eclipse specific applications for Entegra II, including all synoptic pages and ACS and ISS interface. Defined low-level requirements and designed software for the Eclipse specific applications. Supported all phases for the Eclipse certification. DO-178B Level B



Honeywell

• United States
• Appliances, Electrical, and Electronics Manufacturing
• 700 & Above Employee

• Software Engineer

  • Oct 2000 - Mar 2004

  Responsible for the software development of aircraft LCD displays. Electronic Standby Indicator is an Electronic Flight Instrument capable of displaying critical information to the pilot in the event of loss of data from the primary flight displays. Responsible for software design and implementation of all graphics functions. Multi-Function Radar Display is an Electronic Flight Instrument capable of displaying weather radar, NAV/FMS map, terrain, traffic and lightning. Responsible for software design and implementation of Primus Weather Radar display. Electronic Horizontal Situational Indicator (EHSI) is an Electronic Flight Instrument capable of displaying the horizontal situation, GPS map, and lightning and traffic overlays. Responsible for software design, implementation and testing of the Pilot Menu and GPS mapping display. Flight Warning Computer (FWC) monitors aircraft sensors and flight phases to provide proper signals to remote indicators, and warning lights. Project included adding new warnings. Responsible for software requirement, design, implementation and testing. Aural Warning Unit (AWU) monitors aircraft sensors to provide discrete signals to the Engine Instrumentation and Crew Alerting System and female voice and other aural alert signals. Project included adding aural alerts. Responsible for software requirement, design, implementation and testing.



EDS

• Senior Engineering Systems Engineer

  • Sep 1989 - Oct 2000

  Responsible for the software development of advanced and production suspension and braking systems. Designed and developed PC-based instrumentation software used by development and ride-control engineers. Development of software used for testing automotive components. The Leveling Smart Sensor is a low cost, low powered, compact device that levels the vehicle through varying road conditions. Responsible for software design, implementation and testing. Real Time Damping (RTD) is a series of semi-active suspension controllers. Responsible for writing software on the PC used to simulate the outputs of the RTD algorithm and compare with the outputs of production controllers in order to verify their proper operation. Four corner leveling will adjust the ride height of each of the corners based on varying vehicle loads. Responsible for software implementation and testing. Body Control Damping is a low cost, electronically controlled suspension system that is capable of running within a brake controller. Responsible for combining software specifications and code from brakes and suspensions controllers to implement the BCD code. SEI CMM Level 2 Organization.