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The goal of the thesis is to design and synthesize an algorithm for on-board usage, and to analyze its performance with respect to baseline solutions in various scenarios.
Job Responsibility:
Understanding of the sources and dynamical behaviour of spacecraft total angular momentum and its residuum after magnetic desaturation
Familiarization with Model Predictive Control methods
Derivation or usage of suitable mathematical prediction models that are usable in an on-board setting
Synthetisation of a MPC controller and providing a suitable tuning strategy
Implementation of the control algorithm and application to given scenarios
Evaluation and documentation of work
Requirements:
Enrolled full time master student (d/f/m) as Aerospace Engineering, Cybernetics or similar field of study
Very good knowledge of MATLAB / Simulink
Very good knowledge of dynamics and control
English fluent
Nice to have:
German would be an asset
You are a good team player, have excellent communication skills, and are able to work independently
What we offer:
International environment with the opportunity to network globally
Work with modern/diversified technologies
At Airbus, we see you as a valuable team member and you are not hired to brew coffee, instead you are in close contact with the interfaces and are part of our weekly team meetings
Opportunity to participate in the Generation Airbus Community to expand your own network