Semi-analytical optimal control for spacecraft constrained hovering over tumbling object

•Two-layer semi-analytical control optimization for constrained hovering over tumbling object.•A direct method utilizing only state variables as optimization variables.•Satisfy state inequality constraints by state transformation of saturation function.•Avoid numerical integration by analytical solu...

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Bibliographic Details
Published inAdvances in space research
Main Authors Feng, Zhan, Bai, Xue, Jiang, Jun, Zhu, Jun, Xu, Ming
Format Journal Article
LanguageEnglish
Published Elsevier B.V 01.06.2025
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