Corrigendum to “Integrated guidance for Mars entry and powered descent using reinforcement learning and pseudospectral method” (Acta Astronautica (2019) 163(PB) (114–129), (S0094576518313043), (10.1016/j.actaastro.2018.12.033))

Xiuqiang Jiang, Shuang Li, Roberto Furfaro

Research output: Contribution to journalComment/debatepeer-review

Abstract

The authors regret that due to an unintentional paste mistake and typing error, several figures and values of parameters need to be corrected. The corrections are mentioned below (see Figs. 5, 6, 10, and 11): [Figure presented] [Figure presented] [Figure presented] [Figure presented] Below Fig. 11, the third coordinate value of the ‘optimal handover location ri’ is 4.8965. In Table 3, the value of the ‘Maximum dynamic pressure qmax’ is 12 × 103. The authors would like to apologize for any inconvenience caused.

Original languageEnglish (US)
Pages (from-to)323-324
Number of pages2
JournalActa Astronautica
Volume168
DOIs
StatePublished - Mar 2020

ASJC Scopus subject areas

  • Aerospace Engineering

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