Input-output linearized spacecraft formation control via differential drag using relative orbital elements

Research article (Advances in Space Research, 2020) · cited 13× · AI/ML
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Input-output linearized spacecraft formation control via differential drag using relative orbital elements

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Input-output linearized spacecraft formation control via differential drag using relative orbital elements is a scholarly article[1].

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APA 4ort.xyz Knowledge Graph. (2026). Input-output linearized spacecraft formation control via differential drag using relative orbital elements. Retrieved May 24, 2026, from https://4ort.xyz/entity/input-output-linearized-spacecraft-formation-control-via-differential-drag-using-relative-orbital-elements
MLA “Input-output linearized spacecraft formation control via differential drag using relative orbital elements.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/input-output-linearized-spacecraft-formation-control-via-differential-drag-using-relative-orbital-elements.
BibTeX @misc{4ortxyz_input-output-linearized-spacecraft-formation-control-via-differential-drag-using-relative-orbital-elements_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Input-output linearized spacecraft formation control via differential drag using relative orbital elements}}, year = {2026}, url = {https://4ort.xyz/entity/input-output-linearized-spacecraft-formation-control-via-differential-drag-using-relative-orbital-elements}, note = {Accessed: 2026-05-24}}
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