Professional Profile
Systems Engineer with experience in all phases of the software lifecycle. Performed requirements development and analysis, hardware/software integration, and flight software testing and verification.
• Systems Integration and Testing
• Requirements Development & Verification
• DOORS
• Avionics Lab Experience
• Real Time Software Debugging
• Post Data Analysis
• Software processes
• Configuration Management
• Communication with NASA Customers
• Meeting Coordinator and Presenter
• C/C++ experience
Professional Experience
Systems Engineer III
Honeywell, Phoenix, AZ
January 2012 - Present
Responsibilities:
• Next Generation Flight Management System Software Checkout Integration Lead for multiple aircraft platforms
o Create integrated software builds from components modified by various software teams
o Assign, monitor and perform software build checkout tests
o Analyze problems found to identify root cause and report to software development teams
• Software Change Request Analysis
o Recreate software issue on desktop simulation or integrated lab environment
o Identify root cause of the software issue and assign to the appropriate development team for resolution
Software Test Engineer
Lockheed Martin, Denver, CO
November 2010 - December 2011
Responsibilities:
• Flight Software Acceptance & Verification Testing for the Gravity Recovery and Interior Laboratory (GRAIL) mission
o Fault Protection Tests at the Component, Performance, and System levels for the Electrical Power System, Star Tracker, and Safe Mode Executive
o Module level and integrated testing of Operating System, memory read/write functions, and memory integrity tests
o Risk Reduction (regression) Testing
o Tests were performed in a SoftSim environment and scripted using TCL
o Test results determined through analysis of Event Reports and Fault History Table entries in an integrated test report
o Hosted Tabletop, Dry Run, and Final Run Reviews where test data and results were presented to the NASA customer
Systems Integration and Test Engineer
Lockheed Martin, Houston, TX
December 2007 – November 2010
Responsibilities:
• Hardware/Software Integration at the Spacecraft Level for the Pad Abort 1 (PA-1) of the Orion Flight Test Article (FTA)
o Test procedures consisted of a systems checkout of the electrical interfaces of the Space Integrated GPS/INS (SIGI) and Launch Abort System Interface Emulator
o Developed test scripts from interface diagrams
o Authored and executed test proc...
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