Stellenbeschreibung 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.

Mission Analysis and Flight Dynamics Engineer (m/f/d)