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A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint
Research article (Aerospace Science and Technology, 2019) · cited 67× · AI/ML
A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint
Summary
A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint is a scholarly article[1].
Key Facts
A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint's instance of is recorded as scholarly article[2].
References
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Use these citations when quoting this entity in research, articles, AI prompts, or wherever provenance matters. We aggregate Wikidata + Wikipedia + authoritative open-data sources; the stitched, scored, cross-referenced view is what 4ort.xyz contributes.
APA4ort.xyz Knowledge Graph. (2026). A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint. Retrieved May 24, 2026, from https://4ort.xyz/entity/a-novel-non-singular-terminal-sliding-mode-control-based-integrated-missile-guidance-and-control-with-impact-angle-const
MLA“A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/a-novel-non-singular-terminal-sliding-mode-control-based-integrated-missile-guidance-and-control-with-impact-angle-const.
BibTeX@misc{4ortxyz_a-novel-non-singular-terminal-sliding-mode-control-based-integrated-missile-guidance-and-control-with-impact-angle-const_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint}}, year = {2026}, url = {https://4ort.xyz/entity/a-novel-non-singular-terminal-sliding-mode-control-based-integrated-missile-guidance-and-control-with-impact-angle-const}, note = {Accessed: 2026-05-24}}
LLM promptAccording to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint — https://4ort.xyz/entity/a-novel-non-singular-terminal-sliding-mode-control-based-integrated-missile-guidance-and-control-with-impact-angle-const (retrieved 2026-05-24)
