Job Description:
The role is within Flight Control Systems department which is a part of the Aircraft System Integration area within the Engineering Directorate. The purpose of the role is to carry out Software Model-Based Design activities within scope of Flight Control System development for FCS conventional programs (AW169, AW189, AW101, AW249, AW139MKII), Tiltrotor programs (NEXTGEN) and UAV programs.
Main Tasks:
• Analysis of FCS system requirements driving SW design
• Production of FCS SW Model Based Design, in compliance with system level requirements allocated to FCS SW items, using Matlab/Simulink toolchain and/or LHD proprietary tool
• Production of the Model Based Software Requirements Specification and management of their validation/traceability with respect to system requirements allocated to FCS SW items
• Integration of the Model Based Design artifacts in the Simulink Test Environment (STE) and ensure the functionality of the integrated STE
• Management of Configuration Control of the Model Based Design artifacts according to applicable procedures and standards
• Support software integration and system/software test activities in FCS test environment (VDE, RIG, and STE)
• Design analysis, troubleshooting and debugging on simulated or real platform
• Management of design changes throughout development life cycle
• Preparation of technical documentation for reporting or peer/formal reviews
• Management of Technical Design Review presenting Model Based Design to the relevant stakeholders
• Planning and progress reporting
Seniority:
Expert