@inproceedings{c1155586b6214ef8b076e3b14fb031ee,
title = "Optimal linear quadratic guidance law with terminal impact angle constraint",
abstract = "Traditional guidance methods ensure simple algorithm and precision, however, they may create a lower impact angle. In recent years there has been an increasing interest in guidance law in order to improve the impact angle. This paper proposes an optimal guidance law under the constraints of miss distance and impact angle. The approach adopted extensively is called linear quadratic optimal control theory. Simulation results indicate that the damage ability can be increased significantly compared with the proportional navigation law, which improves the performance of modern guided weapons enormously.",
keywords = "Impact angle, Linear quadratic, Oplimal guidance law",
author = "Zhao Jianyu and Yu Jianqiao and Yang Kun",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 29th Chinese Control and Decision Conference, CCDC 2017 ; Conference date: 28-05-2017 Through 30-05-2017",
year = "2017",
month = jul,
day = "12",
doi = "10.1109/CCDC.2017.7978462",
language = "English",
series = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "7095--7098",
booktitle = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",
address = "United States",
}