Company description Civitanavi Systems S.p.A. is a leading player in the design, development and manufacture of high-tech solutions for Navigation, Control and Stabilization Systems, for several applications in Aerospace Defense and Industrial sectors. The application of proprietary methods and technologies, based on FOG (Fiber Optic Gyroscope) and MEMS (Micro Electro-Mechanical Systems) technology, enables the company to best meet the specific needs of its customers. Founded as a start-up in 2012 in Italy, listed company on Euronext Milan since 2022 and now part of Honeywell (acquisition and delisted completed in August 2024). Job Summary The System Engineer will be involved in the design and technical development of inertial navigation systems for both the Industrial and Aerospace & Defense domains. The main tasks will include analyzing customer requirements, generating system architecture, establishing formal system requirements, defining applicable methods for requirements validation, specifying procedures for design verification, supporting proper installation of the product into the target platform, and overall coordination of system development, integration, and qualification/certification activities, alongside continuous communication with the customer on all technical aspects. Responsibilities and duties Support definition and drafting of the System Development Plans in accordance with recognized standards (ARP4754, ARP4761). Organizing and ruling the documentation for program development. Define High-level System Requirements and System Architecture. Flow-down of requirements from system to item level (SW, HW, MECH, etc.). Review of low-level requirements for various subassemblies and components (mechanical parts, electronic boards, optical and opto-electronics components, software and firmware (FPGA) modules, configuration parameters). Static and dynamic analysis of IMU performance. Support the System Test Department in defining System Test procedures and Qualification Plans according to widely recognized standards (ARP-4754, DO-160, MIL-STD-810, MIL-STD-461). Support system integration and testing of INS/AHRS/IMU with complex software and hardware. Review and approve technical design documents and data related to the system under development. Review acceptance test reports, qualification test reports, similarity analysis reports, and all technical studies related to the system under development. Evaluate technical specifications included in the documentation package of the bid/request for proposal (RFP) to contribute to the preparation of the technical proposal and the compilation of the requirements compliance matrix. Qualification and skills Required Skills University degree in Electronics, Opto-Electronics, Aerospace, Mechanical Engineering, Computer Science, Physics or equivalent. 2 years of experience in a similar role. Knowledge of avionics, navigation and related algorithms, control systems theory. Knowledge of main communication interfaces and protocols. Knowledge of relevant System and Safety engineering standards such as ARP-4754, ARP-4761. Knowledge of RTCA DO-160, MIL-STD-810, MIL-STD-461 environmental/EMC test standards. Knowledge of MathWorks MATLAB/Simulink. Familiarity with requirements management tools (preferred IBM Rational DOORS). Familiarity with system safety concepts and reliability assessment (PSSA, SSA, FMECA, FTA, etc.). Ability to work in a team. Ability to work under pressure. Ability to adopt effective communication depending on the audience and context within the technical team. Systematic and organized to manage project documentation and track and archive every detail generated during system development. Capable of performing in-depth investigations of system failures or anomalies with a multidisciplinary approach. Knowledge of English language (at least intermediate level). Preferred Skills Knowledge of reliability prediction standards (preferred MIL-HDBK-217F). Knowledge of model-based design. Knowledge of EASA and ESA documentation governing product qualification/certification. J-18808-Ljbffr