@inproceedings{e545de6af76b4f56ba39d002020244c0,
title = "Design of 3-D discrete sliding mode variable structure guidance law for air missile",
abstract = "Based on kinematics relationship model of missile and target in three-dimensional space, this assignment will extend 2-D plane to realistic 3-D space. Firstly, it will deduce 3-D Guidance Law Model between air missile and maneuvering target. Then this assignment will design suitable discrete sliding mode variable structure guidance law through the robustness characteristic controlled by sliding mode. The guidance features will be subsequently analyzed. Finally, the result will confirm the feasibility of the designed guidance law through the mathematical simulation.",
keywords = "discrete sliding mode guidance law, robustness, three-dimensional space, variable structure",
author = "Le Chang and Zhenghua Liu and Xiaoxiao Zong",
year = "2012",
doi = "10.1109/WCICA.2012.6358241",
language = "英语",
isbn = "9781467313988",
series = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",
pages = "2204--2208",
booktitle = "WCICA 2012 - Proceedings of the 10th World Congress on Intelligent Control and Automation",
note = "10th World Congress on Intelligent Control and Automation, WCICA 2012 ; Conference date: 06-07-2012 Through 08-07-2012",
}