@article{GONG2022, 
author = {Mian GONG and Di ZHOU and Xinguang ZOU},
title = {Saturated super-twisting sliding mode missile guidance},
year = {2022},
journal = {Chinese Journal of Aeronautics},
volume = {35},
number = {10},
pages = {292-300},
keywords = {Highly maneuvering target, Input saturation, Missile guidance control, Robust control, Sliding mode control, Super-twisting algorithm},
url = {https://www.sciopen.com/article/10.1016/j.cja.2021.11.008},
doi = {10.1016/j.cja.2021.11.008},
abstract = {This paper concentrates on developing a missile terminal guidance law against a highly maneuvering target whose maneuvering acceleration is very close to that of the missile or even exceeds the missile normal acceleration in a finite period of time. A new saturated super-twisting algorithm is proposed and applied to the design of missile guidance law. The proposed algorithm has the advantages of simple structure, easy parameter tuning rules and a full utilization of the limit control input. The designed saturated super-twisting sliding mode guidance law is then employed in a missile guidance system. Simulation and its superior performance against strong maneuvering targets is demonstrated.}
}