This project aims to addresses the stability of orbital motion around minor bodies (asteroids or comets) considering uncertainties of the initial state of the spacecraft and also the uncertainties of the model parameters e.g. the mass of the asteroid, rotation errors, etc., with algebraic propagation methods. This position will start no later than end Nov. 2019. Please send your application (including CV, cover letter, Certificate of bachelor and master degree (if applicable) and two reference letters) to [email protected] by 16th Otc. 2019.
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