Experience designing flight critical hardware architecture for an air vehicle. Perform component hardware and software integration, and derive software requirements for control of flight-critical and safety-critical systems Develop and execute component, subsystem, and system level test procedures to verify functionality of the VMS hardware and software. Investigate and resolve system anomalies across multiple engineering disciplines Perform technical planning, analysis, and hardware trade studies to meet requirements. Coordinate and manage suppliers for hardware procurement Experience working with hardware in a hands-on laboratory environment. Ability to troubleshoot hardware and software problems. Experience developing in one or more of the following languages C, C++, Rust and Python. Ability to read and evaluate an electrical schematic. Bachelor's Degree in a Science, Technology, Engineering, or Mathematics (STEM) field from an accredited university with 5 years of related engineering experience OR a master's degree (STEM) with 3 years of related engineering experience OR a PhD Degree (STEM) discipline from an accredited university with a minimum of 0 years of experience. Experience with design, development, and/or integration of the Air Vehicle systems and subsystems listed above Experience with defining electrical and data interfaces (such as MIL-STD-1553, RS-232, ARINC 429, or analog interfaces) Experience with hardware/software integration Bachelor's Degree in a Science, Technology, Engineering, or Mathematics (STEM) field from an accredited university with 9 years of related engineering experience OR a master's degree (STEM) with 7 years of related engineering experience OR a PhD Degree (STEM) with 4 years Must have a current active in-scope DoD Secret security clearance or higher, with the ability to obtain Special Program Access (SAP). Priority given to individuals with a degree in computer, software or electrical / electronic engineering. Extensive experience with design, development, and/or integration of the Air Vehicle systems and subsystems listed above Extensive experience with defining electrical and data interfaces (such as MIL-STD-1553, RS-232, ARINC 429, or analog interfaces) Extensive experience with hardware/software integration, verification & validation Extensive experience with engineering modeling and simulation Experience writing device specific ICD parsing software (e.g. Parsing an inertial measurement unit byte stream to receive appropriate acceleration data) Experience with utilizing lab test equipment (e.g. oscilloscope, multimeter, etc.) Priority given to individuals with a degree in computer, software or electrical / electronic engineering Experience developing within a real-time operating system Experience working with and developing for communication protocols such as, RS-232, RS-485 or MIL-STD-1553. Experience developing within the Linux for ARM environment Excellent oral, written, and interpersonal communication skills Ability to lead a team, organize work, manage time, plan, and prioritize