support the development and analysis of spacecraft systems
assist in the design, analysis, and implementation of GNC algorithms
support GNC mode transition analysis and performance evaluations for spacecraft systems
perform Monte Carlo simulations to quantify system performance and ensure compliance with requirements
develop MATLAB scripts and models to analyze GNC subsystems
integrate simulations with SIMULINK and STK tools
analyze and interpret data from GNC sensors such as IMUs and GPS
collaborate with team members to integrate GNC flight software (FSW)
conduct hardware-in-the-loop (HITL) simulations
document results, provide technical reports, and communicate findings to the team and stakeholders
estimate workloads and prioritize day-to-day tasking under the direction of technical leads

Bachelor’s degree in aerospace engineering, mechanical engineering, electrical engineering, or a related technical field (or equivalent work experience in lieu of degree)
Typically, 2+ years of relevant engineering experience (including academic projects, internships, or research)
Foundational knowledge of statics, dynamics, control systems, and orbital mechanics
Proficiency in MATLAB programming and familiarity with SIMULINK, STK, and version control tools such as GIT/SVN
Basic understanding of GNC sensors like IMUs and GPS and their operating principles
The ability to obtain and maintain a U.S. Security Clearance is required

Guidance, Navigation and Control Engineer II

Key skills