About this role
Your Tasks - Perform Mission Analysis for Earth observation satellites in LEO and GEO. - Analysis and derivation of Mission and System performance parameters - Point of Contact to Subsystem designers for Mission-related requirements and constraints. - Point of Contact to Payload designers and System Engineers (in particular, Operations preparation engineers) for the consolidation of an operational concept related to the payload commanding. - Provide Subsystem designers with the required Mission-related analyses and profiles. - Conception, design, development and validation of SW packages for Mission Analysis and Flight Dynamics purposes. - Development of optimal / suboptimal Attitude Guidance profiles - Computation of nominal mission profiles. - Development of Orbit Control strategies and related SW - Derivation of Mission-related requirements. Your Qualifications - Master’s or doctoral degree or equivalent in Engineering, Physics or Mathematics. - Deep and hands-on knowledge on Orbital Dynamics problems and methods. - Ability and experience to apply theoretical knowledge for the solution of technical problems in Space Flight Dynamics. - Experience in the use of numerical methods for Orbit Determination and Control. - Experience as FD engineer in operational context is a plus. - Good knowledge of satellite Attitude Kinematics and Dynamics. - Knowledge and experience in optimization theory is a plus. - Ability to work in cooperation with Systems and Subsystems Engineers in multidisciplinary teams. - Excellent command in MATLAB and Python. C and System Tool Kit (STK) are a plus.