Output-Feedback Tube Model Predictive Control for Asteroid Circumnavigation and Descent

What is it about?

Future space missions require the development of autonomous guidance and control systems so that the spacecrafts can manoeuvre and take decisions independently. We propose on such method that is has focus on computational simplicity, while also considering restrictions on movement, together with restrictions on thrust. The proposed method can be used to both circumnavigate and land on asteroids and small bodies

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