Dynamic output feedback fuzzy sliding mode learning attitude control for hypersonic flight vehicle with actuator rate constraint

Xiaoxiang Hu, Yuewen Wang, Jingwen Xu, Jingyan Zhao, Bing. Xiao. Dynamic output feedback fuzzy sliding mode learning attitude control for hypersonic flight vehicle with actuator rate constraint. J. Franklin Institute, 363(2):108374, 2026. [doi]

Abstract

Abstract is missing.