About this role

Develop and improve CLaws design and assessment tools using Matlab and C++
Support CLaws, autopilot, and navigation design development for R&D projects
Develop CLaws and systems requirements
Perform V&V for any CLaws updates and/or new designs
Verify and deliver CLaws in accordance with DO‑178B standard and SAE ARP 4754
Design and develop pilot-in-the-loop CLaws based on performance and test pilot assessments
Evaluate CLaws and FBW system failures and stability with analytical methods and flight test data
Support integration of CLAWS into various test rigs and supplier hardware

10 years of pertinent experience in the development of Flight Control Laws for FBW (Fly‑By‑Wire) aircraft
Bachelor’s or master’s degree in Aerospace Engineering; PhD preferred
Expertise in aircraft flight dynamics, aerodynamics, and handling qualities
Proficiency in MATLAB/Simulink and C++ programming
Experience with control systems design (Classical, Modern, SISO/MIMO)
Knowledge of DO-178B, SAE ARP4754, and aerospace software certification standards
Good understanding of control law evaluation techniques and testing procedures
Good understanding of aircraft stability and handling qualities with pilot-in-the-loop
Proficient in programming Matlab scripts and C++ programming
Fluent in written and spoken French and English

Flight Control Laws Designer

Key skills