Develop control laws to meet air vehicle performance, flying qualities and stability margin requirements, both on ground and in flight. Develop air vehicle system linear and non-linear dynamic simulation models and integrate models into software and hardware-in-the-loop simulation environments. Analyze air vehicle flight test data and support flight test activities. Bachelors in Science, Technology, Engineering or Math (STEM) and at least 12 years of experience, a Master's Degree in STEM with 10 years of experience, or a PhD Degree with 7 years of experience. Excellent communication, analysis and problem-solving skills Knowledge of fixed-wing aircraft flight dynamics Experience using linear control principles and tools to design feedback control systems Experience analyzing non-linear simulations of aircraft closed-loop dynamics Experience using MATLAB to create, process, analyze, and visually represent data Active / in-scope DoD Secret Clearance Proficient in MATLAB/Simulink Experience designing control laws for fixed wing aircraft and performing handling qualities analysis Working knowledge of MIL-STD-1797 flying qualities requirements Active / in-scope DoD Top Secret Clearance