@inproceedings{af749beaac67435c98a257ba0813bf43,
title = "Design of 3-dimensional guidance law of missile based on discrete sliding mode",
abstract = "In this article, a new approach to design discrete-time sliding-mode guidance laws is presented based on the target-missile relative motion equation in three -dimensional space. This method significantly reduced system chattering and could be easily achieved on engineering. Furthermore, effectiveness of the proposed guidance laws is demonstrated through simulation by comparing with the traditional proportional guidance laws.",
keywords = "3-dimensional space, Discrete time, Guidance laws, Variable structure",
author = "Nuan Wen and Liu, \{Zheng Hua\} and Le Chang",
year = "2013",
doi = "10.4028/www.scientific.net/AMR.816-817.976",
language = "英语",
isbn = "9783037858677",
series = "Advanced Materials Research",
pages = "976--980",
booktitle = "Manufacturing Science and Technology (ICMST2013)",
note = "4th International Conference on Manufacturing Science and Technology, ICMST 2013 ; Conference date: 03-08-2013 Through 04-08-2013",
}