The design team is composed of high skilled managers, engineers and technicians having previous experiences in International Aeronautic Programs and able to develop proprietary Unmanned Air Vehicle with top in the class performances.
Autopilot and FCC proprietary design. Dynamic analysis and control laws design for aircraft on-board systems. Thermo-fluid analysis. SW development via model-based design, compliant with aeronautical standards – DO-178C. HW & FW development. Reliability and safety analysis. FEM structural and aero-servo-elastic analysis.
Carbon fiber structure in order to guarantee minimum weight and high structural characteristics. Stress analysis carried out with aerodynamic simulations allow to minimize the radar cross section.
To reduce in advance the risk in the flight test campaign, we developed hardware-in-the-loop and real-time software simulators, integrated in the test rigs and in the complete aircraft iron bird.