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This paper presents verification of a modeling and simulation for a Spacecraft (SC) attitude and orbit control system. Detailed formulation of coupled SC orbital and attitude equations of motion is performed in order to achieve accepted accuracy to m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::90a97f757bf0f3eb924d81a5a47df642
Publikováno v:
AIAA SPACE 2016.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13c00a6424a3d8984335306436a8650b
https://doi.org/10.2514/6.2016-5552
https://doi.org/10.2514/6.2016-5552
