Corrie Spaulding

Principal Hardware Engineer at EXB Solutions, Inc
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Contact Information
us****@****om
(386) 825-5501
Location
McKinney, Texas, United States, US

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Experience

    • United States
    • Software Development
    • 1 - 100 Employee
    • Principal Hardware Engineer
      • Mar 2023 - Present

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Principal Electrical Engineer
      • May 2019 - Mar 2023

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Sr. Electrical Engineer
      • Mar 2018 - Jun 2019

    • France
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Senior Electrical Engineer
      • Jan 2016 - Mar 2018

      Auto Throttle Control Quadrant – Embraer 505 Phenom • Developed master engineering schedule to adhere to DO-254, ARP-4754A and DO-178C • Developed system architecture to comply with safety critical application • Developed system requirements and decomposed to hardware requirements. Dimming Control and Power System – COMAC ARJ21 (2016-2017) • Designed DC/DC power delivery system for power delivery to lighting panels • Aided in the design of a programmable solution for generating a non-linear dimming curve • Developed system level requirements and statement of work to scope the program. DO-254 Process Development – Company Process Development (2016-2017) • Developed DO-254 internal process from program inception through production transition • Developed standard templates for PHAC, HDP, HVVP, PAP, and CMP Show less

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Senior Electrical Engineer
      • Feb 2013 - Dec 2015

      Interceptor Interface Module Flight – Embraer Legacy 550 (2013-2014) • Defined and Managed Hardware Requirements through design development life-cycle • Analog and Digital Analysis to provide verification of hardware level requirements • Provided guidance on DO-254 and ARP-4754A Guidelines for hardware requirements capture • Developed a HRD review process that adhered to approved System Development Process Interceptor Interface Module Flight - Bombardier CSeries (2013-2014) • Company wide process development for hardware life-cycle to meet the objectives of ARP-4754A Guidelines • Analog and Digital Analysis to provide root cause analysis that lead to corrective action to design concerns • Reverse engineered previously developed hardware to produce a hardware design document • Manage hardware development from system architecture through requirements capture to verification and certification Show less

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Electrical Engineer II
      • Jul 2010 - Feb 2013

      Weather Radar Processing System• Lead lightning protection circuit card design from requirements development to final design.• Implemented FPGA design for integrated test solution for various applications• Developed verification system and procedures to meet federal regulation• Developed hardware level requirements to meet system level requirements and customer requests.• Designed digital signal processing system designed to interact with aircraft I/O• Implemented CPLD design for synchronous rectification used in system power supply design Show less

    • Electrical Engineer
      • Jul 2007 - Jul 2010

      Adaptive Flight Display - Gulfstream G200 and Bombardier CSeries(2007-2010)• Designed processing system according to DO-254 avionics design assurance for Adaptive Flight Display• Aided in development of ASIC/FPGA memory controller to be used on multiple platforms.• Developed embedded test software to be used verification of Processor and Ethernet module.• Developed power sequencing system and firmware for programmable power monitoring system.• Developed requirements to adhere to DO-254 Design Assurance Level A for complex devices.Common Computing Module - Gulfstream G200 and Bombardier CSeries (2008-2010)• Developed requirements for FPGA designed to DO-254 Design Assurance Level A.• Developed test procedures to verify an FPGA to DO-254 Design Assurance Level A.• Developed Design Implementation Guide document for FPGA used for CRC Generation.• Analyzed cache usage for PowerPC 7448 Processor using Average Memory Access Time Model.Graphics Generator Module - Boeing 787 Dreamliner(2007)• Aided in development of solutions to FAA EMI and Vibration Qualifications that led to qualification of the product.• Part and PCB level debug of integrated processing and graphics systems which lead to more effective testing.• Developed Processing System and memory requirements and verification procedures to adhere to DO-254.• Aided in embedded software development for system level debug to be used in factory development Show less

Education

  • University of Houston
    Bachelors of Science, Electrical Engineering
    2001 - 2007

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