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

Junjie Lu; Zhongjie Meng; Bo Liu

doi:10.1016/j.actaastro.2026.04.038

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

Junjie Lu
, Zhongjie Meng
, Bo Liu

航天学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 评论/辩论

摘要

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.”

源语言	英语
页（从-至）	627
页数	1
期刊	Acta Astronautica
卷	246
DOI	https://doi.org/10.1016/j.actaastro.2026.04.038
出版状态	已出版 - 9月 2026

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10.1016/j.actaastro.2026.04.038

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

abstract = "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.”",

author = "Junjie Lu and Zhongjie Meng and Bo Liu",

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AU - Liu, Bo

PY - 2026/9

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N2 - 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.”

AB - 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.”

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M3 - 评论/辩论

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ER -

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

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