Highlights Optimal integrated guidance for Mars entry and powered descent is designed. Integrated guidance is produced in a collaborative optimization manner. Mars entry and powered descent guidance are combined via optimal handover. Optimal handover is achieved using reinforcement learning approach.
Corrigendum to “Integrated guidance for Mars entry and powered descent using reinforcement learning and pseudospectral method” [Acta Astronaut. (2019) in press, doi: 10.1016/j.actaastro.2018.12.033]
Acta Astronautica ; 168 ; 323-324
2019-08-16
2 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Optimal nonlinear feedback guidance algorithm for Mars powered descent
Online Contents | 2015
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