@inproceedings{062a3776089e49308d11ed478421dfac,
title = "An observer-based missile guidance law",
abstract = "Nonlinear sliding mode guidance laws with finite time convergence are derived for the missile interception in this paper. The proposed guidance laws guarantee that the missile can intercept a maneuverable target with unknown target acceleration. Specially, the control design consists of the estimation of the target acceleration by extended state observer (ESO) and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.",
keywords = "ESO, Finite-time control, Guidance law, Sliding mode control",
author = "Zheng Zhu and Yuanqing Xia and Mengyin Fu and Shuo Wang",
year = "2011",
doi = "10.1109/CCDC.2011.5968387",
language = "English",
isbn = "9781424487363",
series = "Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011",
pages = "1282--1287",
booktitle = "Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011",
note = "2011 Chinese Control and Decision Conference, CCDC 2011 ; Conference date: 23-05-2011 Through 25-05-2011",
}