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Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS)
Research article (Aerospace Science and Technology, 2018) · cited 67× · AI/ML
Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS)
Summary
Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS) is a scholarly article[1].
Key Facts
Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS)'s instance of is recorded as scholarly article[2].
References
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APA4ort.xyz Knowledge Graph. (2026). Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS). Retrieved May 24, 2026, from https://4ort.xyz/entity/nonsingular-terminal-sliding-mode-control-technique-for-attitude-tracking-problem-of-a-small-satellite-with-combined-ene
MLA“Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS).” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/nonsingular-terminal-sliding-mode-control-technique-for-attitude-tracking-problem-of-a-small-satellite-with-combined-ene.
BibTeX@misc{4ortxyz_nonsingular-terminal-sliding-mode-control-technique-for-attitude-tracking-problem-of-a-small-satellite-with-combined-ene_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS)}}, year = {2026}, url = {https://4ort.xyz/entity/nonsingular-terminal-sliding-mode-control-technique-for-attitude-tracking-problem-of-a-small-satellite-with-combined-ene}, note = {Accessed: 2026-05-24}}
LLM promptAccording to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): Nonsingular terminal sliding mode control technique for attitude tracking problem of a small satellite with combined energy and attitude control system (CEACS) — https://4ort.xyz/entity/nonsingular-terminal-sliding-mode-control-technique-for-attitude-tracking-problem-of-a-small-satellite-with-combined-ene (retrieved 2026-05-24)
