Abstract ĭetta dokument presenterar arbetet och resultaten som erhållits inom ramen för examensarbetet som genomförts från februari 2020 till juli 2020 på DLA/SDT/SPC-avdelningen. This gives strong evidences that the guidance strategy is reliable as well as performant and that it can be part of the CALLISTO GNC system. The yielded results are satisfying in the sense that all specifications are fulfilled by the strategy in order to perform a safe touchdown. This strategy has been implemented and validated by running numerous simulations. The guidance strategy is based on solving a real time convex optimization problem. This master thesis was realized under the supervision of CNES engineer Eric Bourgeois and it is part of the KTH Master of Science in Aerospace Engineering.Ī 3D guidance strategy for the landing phase of a reusable launcher has been elaborated in order to make the vehicle land safely with a high accuracy. This document presents the work and the results obtained in the frame of the master thesis that has been conducted from February 2020 to July 2020 in the DLA/SDT/SPC service. Konvexa styrstrategier för landning av återanvändbara raketer (Swedish)
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