8+ years designing and fielding flight control systems for fixed-wing aircraft or high-performance UAVs, including flight test
Deep knowledge of flight dynamics, stability/controllability, and actuator/sensor modeling
Proficiency in modern C++ for embedded real-time implementations; strong MATLAB/Python for modeling, ID, and analysis
Demonstrated ownership of verification workflows (SIL/HIL), requirements traceability, and safety reviews
Familiarity with modern software workflows (git, code review, issue tracking) and data/telemetry analysis
Responsibilities
Define control system architecture and requirements for fixed-wing vehicles (primary flight control, envelope protection, autothrottle/energy mgmt, and mode logic)
Design and implement control laws accounting for actuator limits, time delays, and sensor noise
Lead system identification and aerodynamic model development from wind-tunnel, CFD, and flight-test data; build accurate linearizations
Develop fault-tolerant and reconfiguration strategies (sensor/actuator FDI, control allocation, redundancy mgmt) with graceful degradation
Own verification & validation: SIL/HIL campaigns, Monte Carlo, and flight-readiness criteria; establish performance dashboards
Drive flight-test planning and execution; analyze logs, tune controllers, and iterate safely and quickly
Mentor the controls team, set technical standards, conduct design/code reviews, and influence roadmap and milestones