Home ›
Entities
› academia
› Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control
Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control
Research article (Aerospace Science and Technology, 2022) · cited 58× · AI/ML
Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control
Summary
Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control is a scholarly article[1].
Key Facts
Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control's instance of is recorded as scholarly article[2].
References
Programmatic citations — every numbered marker resolves to a verifiable graph row below.
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). Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control. Retrieved May 24, 2026, from https://4ort.xyz/entity/impact-angle-constrained-integrated-guidance-and-control-for-supersonic-skid-to-turn-missiles-using-backstepping-with-gl
MLA“Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/impact-angle-constrained-integrated-guidance-and-control-for-supersonic-skid-to-turn-missiles-using-backstepping-with-gl.
BibTeX@misc{4ortxyz_impact-angle-constrained-integrated-guidance-and-control-for-supersonic-skid-to-turn-missiles-using-backstepping-with-gl_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control}}, year = {2026}, url = {https://4ort.xyz/entity/impact-angle-constrained-integrated-guidance-and-control-for-supersonic-skid-to-turn-missiles-using-backstepping-with-gl}, note = {Accessed: 2026-05-24}}
LLM promptAccording to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): Impact angle-constrained integrated guidance and control for supersonic skid-to-turn missiles using backstepping with global fast terminal sliding mode control — https://4ort.xyz/entity/impact-angle-constrained-integrated-guidance-and-control-for-supersonic-skid-to-turn-missiles-using-backstepping-with-gl (retrieved 2026-05-24)
