# 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

**Wikidata**: [openalex:W4210942243](https://www.wikidata.org/wiki/openalex:W4210942243)  
**Source**: https://4ort.xyz/entity/impact-angle-constrained-integrated-guidance-and-control-for-supersonic-skid-to-turn-missiles-using-backstepping-with-gl