Corrigendum to “Relative attitude-orbit gain-adapting enhanced coupling control for underactuated spacecraft” [Acta Astronaut. 246 (2026) 83–95]

The authors regret that in the originally published article, the citation of reference [14] was incorrect. The sentence originally read: “Kojima et al. [14] validated the feasibility of using two skewed control moment gyroscopes and designed a feedback control method based on real-time optimization.”