• Developed code to decode various product from the ADS-B stream, which is part of the FAA's NextGen project. Most of the FIS-B (Flight Information Services including many weather products), and TIS-B (Traffic Information Service) are being decoded.• Responsible for implementing and integrating the XM Weather products into the EFD1000 MFD display. This included NEXRAD displays, METARs, SIGMETS, AIRMETS, and more.• Designed and implemented the Synthetic Vision component for the EFD1000, displaying a 3D representation of the terrain, obstacles, and airports to the pilots, as well as providing terrain alerts.• Reverse-engineered portions of the Garmin 430W/530W crossfill serial bus protocol and their database format to allow flight plans to be sent to the Garmin from the EFD1000 by emulating the Garmin.

• As Senior Software Architect, responsible for overseeing the development of the avionics software that was developed in house. This includes requirements and algorithms used throughout the avionics.• Responsible for getting the ACS (Aircraft Computer System) ready for first flight, then Lead of the group to get the software ready for TC (Total Cert). This included writing requirements (SRS, SRD, SDD), developing the code, integrating the code on the aircraft, and helping with certification.• Responsible for Flaps and Landing Gear Requirements (SRS, SRD, SDD) and Software. This included Integration and testing, and troubleshooting control laws, mechanical, and electrical issues.• Brought in to assist other companies in troubleshooting (Electronic Circuit Breakers, AHARS), optimizations (MFD and PFD displays), and Verification (Autopilot) of other systems.

• As Software Lead and Senior Software Architect, responsible for overseeing the development of the avionics software that was developed in house for use on the Eclipse 500. This required managing a small team of bright engineers from initial requirements through certification. • Lead the group responsible for getting the ACS (Aircraft Computer System) ready for first flight, through TC (Total Cert). This included writing requirements (SRS, SRD, and SDD), developing the code, integrating the code on the aircraft, and working on certification.---- Optimized / Redesigned the software architecture of the ACS to allow more functionality and better define a clear System / Application boundary.• Responsible for Flaps and Landing Gear Requirements (SRS, SRD, SDD) and Software. This included Integration and testing, and troubleshooting control laws, mechanical, and electrical issues.---- System was a software control PWM running multiple layers of control loops (Current control loop, Speed control loop, and Position control loop). The Position control maintained synchronization between four Flaps actuators so they were always within 0.1 inches of each other throughout the entire range of motion.---- System was designed with many safety monitors and checks, including being SEU tolerant. This included key values being stored redundantly, memory checked periodically for changes, and state values assigned such that a single bit could not change to another valid state. • Brought in to assist other companies in troubleshooting (Electronic Circuit Breakers, AHARS), optimizations (MFD and PFD displays), and Verification (Autopilot) of other systems.