Previous experience modelling, analyzing and controlling rotary-wing aircrafts.
Experience implementing GNC Software utilizing Model-Based Design best practices.
Familiar with common flight control stability and performance requirement sources (Mill-STD-1797, ADS-33).
Familiarity with aircraft software and hardware certification process (DO-178C & DO-254).
Familiarity with safety critical coding standards (MISRA C).
Experience with flight testing of highly control system dependent configurations of rotary-wing and fixed-wing unmanned systems.
An Ultralight or PPL pilot license.
4+ years of hands-on experience designing, implementing and deploying GNC algorithms on large-scale aerial platforms.
Strong background in control analysis, design, and implementation of embedded systems, with proficiency in programming languages and tools such as Matlab/Simulink, C, C++ and Python.
Proven ability to identify, model and simulate complex aerial systems.
Familiarity with common system engineering process, specifically ARP4754.
Experience designing and managing complex aerospace systems, integrating various components such as hardware, software, and control systems.
Preparation and support of flight test activities, analysis of flight test results.
Experience with Software in the Loop (SILS) and Hardware in the Loop (HILS) software validation.
Strong desire to work in a dynamic and fast-paced environment.
Target-oriented work style with strong analytic problem-solving skills required.